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Aerodynamic heating

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Filed under: Aerodynamic heating

Wood-based paneling as thermal barriers. (U.S. Dept. of Agriculture, Forest Service, Forest Products Laboratory, 1982), by Robert H. White and Forest Products Laboratory (U.S.) (page images at HathiTrust)
Thermal effects on static aeroelastic stability and control. (Wright Air Development Center, Air Research and Development Command, U. S. Air Force, 1959), by Bell Aircraft Corp (page images at HathiTrust)
Instrumentation for magnetoaerodynamic heat transfer. (Physical Research Laboratory, Space Technology Laboratories, 1960), by Richard W. Ziemer (page images at HathiTrust)
Performance improvement of arc heaters for aerodynamic wind tunnels (Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, 1965), by R. C. Eschenbach, E. F. Stresino, and J. R. McLeod (page images at HathiTrust)
Theoretical analysis of the downstream influence of stagnation point mass transfer (Wright-Patterson Air Force Base, Ohio, Aeronautical Systems Division, Air Force Systems Command, U.S. Air Force, 1961., 1961), by Robert J. Cresci, United States. Air Force. Systems Command. Aeronautical Systems Division, Polytechnic Institute of Brooklyn, and United States. Wright Air Development Division (page images at HathiTrust)
Aerodynamic heating of parachutes (Wright Air Development Center, Air Research and Development Command, U.S. Air Force, 1957), by Cornell University. Department of Engineering Mechanics and Materials, F. Frank, S. W. Liu, and A. L. Ruoff (page images at HathiTrust)
Helium injection into the boundary layer at an axisymmetric stagnation point (Aeronautical Research Laboratory, Office of Aerospace Research, U. S. Air Force, 1961), by Herbert Fox and Paul Andrew Libby (page images at HathiTrust)
Recent developments connected with the hypersonic facility of the Polytechnic Institute of Brooklyn. Pt. I: Tests of the compression heater. Pt. II: Aspects of the design, construction and installation of a multiple-outlet collector for the convection heater (Wright-Patterson Air Force Base, Ohio : Wright Air Development Division, Air Research and Development Command, United States Air Force, 1959., 1959), by Sergio R. Panunzio, Aerospace Medical Laboratory, United States. Wright Air Development Division, United States. Air Force. Air Research and Development Command, and Polytechnic Institute of Brooklyn (page images at HathiTrust)
A study of the overall problems of the true-temperature, hypersonic wind tunnel having semi-continuous operation and the preferred methods of solution. (Purdue University, School of Aeronautical Engineering, 1959), by George M. Palmer (page images at HathiTrust)
Study of infrared emission in heated air; annual report, July 1960-June 1961 (Cornell Aeronautical Laboratory, 1961), by Walter H. Wurster and Paul V. Marrone (page images at HathiTrust)
A 50-megawatt arc heater: scaling parameters and performance prediction (AF Flight Dynamics Laboratory, Research and Technology Division, Air Force systems Command, 1964), by Richard T. Smith and Joseph P. Doyle (page images at HathiTrust)
An experimental study of the effect of mass injection at the stagnation point of a blunt body (Guggenheim Aeronautical Laboratory, California Institute of Technology, 1958), by Howard K. McMahon (page images at HathiTrust)
Optimum shape for transpiration-cooled nosetip of a re-entry vehicle (Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, 1978), by Kevin E. Yelmgren (page images at HathiTrust)
High temperature radome design techniques. (Cornell Aeronautical Laboratory, 1960), by Godfrey F. Buranich (page images at HathiTrust)
Aerothermal tests of quilted dome models on a flat plate at a Mach number of 6.5 (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1988), by Christopher E. Glass, L. Roane Hunt, and Langley Research Center (page images at HathiTrust)
A review of high-speed, convective, heat-transfer computation methods (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989), by Michael E. Tauber and United States. National Aeronautics and Space Administration. Office of Management (page images at HathiTrust)
Surface flow and heating distributions on a cylinder in near wake of Aeroassist Flight Experiment (AFE) configuration at incidence in Mach 10 air (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), by William L. Wells and Langley Research Center (page images at HathiTrust)
Aerodynamic pressure and heating-rate distributions in tile gaps around chine regions with pressure at a Mach number of 6.6 (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), by L. Roane Hunt, Kristopher K. Notestine, and Langley Research Center (page images at HathiTrust)
Tests of aerodynamically heated multiweb wing structures in a free jet at mach number 2 : five aluminum-alloy models of 20-inch chord with 0.064-inch-thick skin, 0.025-inch-thick webs, and various chordwise stiffening at 2° angle of attack (National Aeronautics and Space Administration, 1960), by Donald H. Trussell, Robert G. Thomson, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Experimental aerodynamic heating of simulated space shuttle tiles in laminar and turbulent boundary layers with variable flow angles at a nominal Mach number of 7 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), by Don E. Avery and Langley Research Center (page images at HathiTrust)
Experimental investigation at Mach 8 of the effects of projections and cavities on heat transfer to a model of the Viking aeroshell (National Aeronautics and Space Administration ;, 1974), by Theodore R. Creel and Langley Research Center (page images at HathiTrust)
Aerothermal tests of spherical dome protuberances on a flat plate at a Mach number of 6.5 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), by Christopher E. Glass, L. Roane Hunt, and Langley Research Center (page images at HathiTrust)
Trajectory characteristics and heating of hypervelocity projectiles having large ballistic coeffients (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), by Michael E. Tauber and Ames Research Center (page images at HathiTrust)
The use of interactive graphic displays for interpretation of surface design parameters (U.S. National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), by Noel A. Talcott, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
Analysis of gap heating due to stepped tiles in the shuttle thermal protection system (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), by D. H. Petley and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
Flight vehicle thermal testing with infrared lamps (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by Roger A. Fields and Dryden Flight Research Facility (page images at HathiTrust)
Low-cycle fatigue of thermal-barrer coatings at 982⁰ C (National Aeronautics and Space Administration, Scientific and Technical Information Service ;, 1978), by Albert Kaufman, Alfred J. Nachtigall, Curt H. Liebert, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
Analysis of metal temperature and coolant flow with a thermal-barrier coating on a full-coverage-film-cooled turbine vane (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by Peter L. Meitner, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, and Propulsion Laboratory (U.S.) (page images at HathiTrust)
Durability of zirconia thermal-barrier ceramic coatings on air-cooled turbine blades in cyclic jet engine operation (National Aeronautics and Space Administration ;, 1976), by Lewis Research Center, Curt H. Liebert, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Optimum element density studies for finite-element thermal analysis of hypersonic aircraft structures (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), by William L. Ko, Kyle M. Muramoto, Timothy Olona, and Dryden Flight Research Facility (page images at HathiTrust)
Heat-transfer distributions on a 0.013-scale shuttle solid rocket booster at Mach 3.70 and angles of attack from 0 ̊to 180 ̊ (National Aeronautics and Space Administration ;, 1976), by Milton Lamb, Robert L. Stallings, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Pressure and heating-rate distributions on a corrugated surface in a supersonic turbulent boundary layer (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1977), by James Wayne Sawyer and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
The use of computer-generated color graphic images for transient thermal analysis (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), by C. L. W. Edwards, James B. Hall, Frances T. Meissner, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
Surface recession characteristics of a cryogenic insulation subjected to arc-tunnel heating (National Aeronautics and Space Administration ;, 1975), by C. M. Pittman, Ronald D. Brown, and Langley Research Center (page images at HathiTrust)
Industry tests of NASA ceramic thermal barrier coating (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), by Curt H. Liebert, Francis S. Stepka, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
Exploratory investigation of two resin-matrix composites subjected to arc-tunnel heating (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), by C. M. Pittman, Ronald D. Brown, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
Aerodynamic heating to the gaps and surfaces of simulated reusable-surface-insulation tile arrays in turbulent flow at Mach 6.6 (National Aeronautics and Space Administration ;, 1975), by Irving Weinstein, Andrew J. Chapman, Don E. Avery, and Langley Research Center (page images at HathiTrust)
Further industrial tests of ceramic thermal-barrier coatings (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), by Curt H. Liebert, Stanley R. Levine, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
In-flight boundary-layer measurements on a hollow cylinder at a Mach number of 3.0 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), by Robert D. Quinn, Leslie Gong, Hugh L. Dryden Flight Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
Low-cycle fatigue evaluation for regeneratively cooled panels (National Aeronautics and Space Administration ;, 1971), by C. E. Richard, Langley Research Center, AiResearch Manufacturing Company of Los Angeles (Calif.), and United States National Aeronautics and Space Administration (page images at HathiTrust)
Optimization of the NiCrAl-Y/Zr0₂-Y₂O₃ (Lewis Research Center, 1985), by Stephan Stecura and Lewis Research Center (page images at HathiTrust)
An experimental investigation of base heating on typical Mars entry body shapes (National Aeronautics and Space Administration ;, 1971), by O. L. Zappa, William G. Reinecke, Langley Research Center, and Avco Corporation. Systems Division (page images at HathiTrust)
Flight test aerodynamic heating data for the afterbody of the Project Mercury spacecraft with comparisons to available prediction methods (National Aeronautics and Space Administration] ;, 1967), by J. D. Murphy, Project Mercury (U.S.), Manned Spacecraft Center (U.S.), Lockheed Missiles and Space Company, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Thermal-structural combined loads design criteria study (National Aeronautics and Space Administration ;, 1972), by V. Deriugin, Langley Research Center, and Boeing Company (page images at HathiTrust)
Thermal and structural tests of a hydrogen cooled panel (National Aeronautics and Space Administration ;, 1972), by C. E. Richard, Langley Research Center, and AiResearch Manufacturing Company of Los Angeles (Calif.) (page images at HathiTrust)
Actively cooled plate fin sandwich structural panels for hypersonic aircraft (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), by L. M. Smith, C. S. Beuyukian, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
Effects of mach number and wall-temperature ratio on turbulent heat transfer at mach numbers from 3 to 5 (U.S. G.P.O.], 1959), by Thorval Tendeland (page images at HathiTrust)
NASA TR R-118 (National Aeronautics and Space Administration :, 1961), by Nathaniel B. Cohen and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
NASA TR R-159 (National Aeronautics and Space Administration ;, 1963), by John T. Howe, John R. Viegas, and United States National Aeronautics and Space Administration (page images at HathiTrust)
NASA TN D-2064 (National Aeronautics and Space Administration, 1963), by Fred A. Demele, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
Prospects for obtaining aerodynamic heating results from analysis of meteor flight data (National Aeronautics and Space Administration :, 1964), by H. Julian Allen, Nataline A. James, and Ames Research Center (page images at HathiTrust)
Exploratory investigation of several coated and uncoated metal, refractory, and graphite models in a 3800° F stagnation temperature air jet (National Aeronautics and Space Administration, 1960), by Otto F. Trout and Langley Research Center (page images at HathiTrust)
NASA TN D-3661 (National Aeronautics and Space Administration :, 1966), by Stanley H. Scher, Irene G. Young, James C. Dunavant, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust; US access only)
NASA TN D-5160 (National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), by Howard W. Stone, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Panel flutter tests on full-scale X-15 lower vertical stabilizer at Mach number of 3.0 (National Aeronautics and Space Administration, 1962), by Herman L. Bohon, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
Shielding stagnation surfaces of finite catalytic activity by air injection in hypersonic flight (National Aeronautics and Space Administration, 1959), by Paul M. Chung and Ames Research Center (page images at HathiTrust)
NASA TN D-4065 (National Aeronautics and Space Administration ;, 1967), by Ronald C. Smith, Alan D. Levin, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Effect of two-dimensional multiple sine-wave protrusions on the pressure and heat-transfer distributions for a flat plate at Mach 6 (National Aeronautics and Space Administration ;, 1968), by Aubrey M. Cary, E. Leon Morrisette, and Langley Research Center (page images at HathiTrust)
Flutter at very high speeds (National Aeronautics and Space Administration, 1961), by Harry L. Runyan, Homer G. Morgan, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
A flight measurement of optical radiation from shock-heated air by using a Trailblazer II vehicle (National Aeronautics and Space Administration ;, 1968), by Lloyd S. Keafer, Ernest E. Burcher, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
Low-perigee aerodynamic heating during orbital flight of an Atmospheric Explorer (National Aeronautics and Space Administration ;, 1976), by Paul S. Caruso, Charles R. Naegeli, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Aerodynamic heating in large cavities in an array of RSI [reusable surface insulation] tiles (National Aeronautics and Space Administration ;, 1977), by L. Roane Hunt, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Downstream influence of swept slot injection in hypersonic turbulent flow (National Aeronautics and Space Administration ;, 1977), by Jerry N. Hefner, Dennis M. Bushnell, Aubrey M. Carey, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
NASA TN D-4720 (National Aeronautics and Space Administration ;, 1968), by Fred R. DeJarnette, Ruby M. Davis, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
NASA TN D-5418 (National Aeronautics and Space Administration ;, 1969), by J. Wayne Keyes, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
The aerothermodynamic environment of the Apollo command module during suborbital entry (National Aeronautics and Space Administration ;, 1972), by Dorothy B. Lee, Winston D. Goodrich, and Manned Spacecraft Center (U.S.) (page images at HathiTrust)
Calculation of laminar heat transfer to the windward surfaces of straight wing shuttle vehicles at high angle of attack and with yaw (National Aeronautics and Space Administration ;, 1972), by C. C. Pappas, United States National Aeronautics and Space Administration, and Ames Research Center (page images at HathiTrust)
NASA TN D-5356 (National Aeronautics and Space Administration ;, 1969), by Robert W. Graham, Donald R. Boldman, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Investigation of aerodynamic effects of external combustion below flat-plate model in 10- by 10-foot wind tunnel at Mach 2.4 (National Aeronautics and Space Administration, 1960), by Robert G. Dorsch, Murray Dryer, Harrison Allen, and Lewis Research Center (page images at HathiTrust)
A study of the aerodynamic characteristics of a fixed geometry paraglider configuration and three canopies with simulated variable canopy inflation at a mach number of 6.6 (National Aeronautics and Space Administration :, 1962), by Jim A. Penland and United States National Aeronautics and Space Administration (page images at HathiTrust)
Motion and heating during atmosphere reentry of space vehicles (National Aeronautics and Space Administration, 1960), by Thomas J. Wong, Robert E. Slye, Glen Goodwin, and Ames Research Center (page images at HathiTrust; US access only)
Effect of geometry variations on lee-surface vortex-induced heating for flat-bottom three-dimensional bodies at Mach 6 (National Aeronautics and Space Administration ;, 1973), by Jerry N. Hefner and Lanley Research Center (page images at HathiTrust)
NASA TN D-3300 (National Aeronautics and Space Administration :, 1966), by Reeves P. Cochran, Robert W. Cubbison, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
Experimental investigation of Mach 3 cruise heating simulations on a representative wing structure for flight-loads measurement (National Aeronautics and Space Administration, 1972), by Roger A. Fields, Richard C. Monaghan, Frank V. Olinger, United States National Aeronautics and Space Administration, and NASA Dryden Flight Research Center (page images at HathiTrust)
Experimental boundary-layer edge Mach numbers for two space shuttle orbiters at hypersonic speeds (National Aeronautics and Space Administration, 1972), by George C. Ashby, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
Interference heating from interactions of shock waves with turbulent boundary layers at Mach 6 (National Aeronautics and Space Administration ;, 1974), by Charles B. Johnson, Louis G. Kaufman, and Langley Research Center (page images at HathiTrust)
Radiative heat transfer during atmosphere entry at parabolic velocity (National Aeronautical and Space Administration, 1961), by Kenneth K. Yoshikawa, Bradford H. Wick, United States National Aeronautics and Space Administration, and Ames Research Center (page images at HathiTrust)
Preliminary studies of manned satellites wingless configuration : nonlifting (National Aeronautics and Space Administration :, 1962), by Maxime A. Faget, James J. Buglia, Benjamine J. Garland, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Calculated effective thermal conductivities of honeycomb sandwich panels (National Aeronautics and Space Administration :, 1959), by Robert T. Swann and United States National Aeronautics and Space Administration (page images at HathiTrust)
Experiments to study strain-gage load calibrations on a wing structure at elevated temperatures (National Aeronautics and Space Administration ;, 1973), by Richard C. Monaghan, Roger A. Fields, and Flight Research Center (U.S.) (page images at HathiTrust)
Experimental evaluation of 3 types of thermal protection materials at moderate heating rates and high total heat loads (National Aeronautics and Space Administration, 1963), by Andrew J. Chapman, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
NASA TN D-3871 (National Aeronautics and Space Administration :, 1967), by James C. Dunavant, Howard W. Stone, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
Investigation of aluminum phosphate coatings for thermal insulation of airframes (National Aeronautics and Space Administration, 1959), by A. G. Eubanks, D. G. Moore, and United States. National Bureau of Standards (page images at HathiTrust)
Investigation of the flow over a spiked-nose hemisphere-cylinder at a Mach number of 6.8 (National Aeronautics and Space Administration, 1959), by Davis H. Crawford and Langley Research Center (page images at HathiTrust)
Optimum design of insulated tension members subjected to aerodynamic heating (National Aeronautics and Space Administration, 1959), by John R. Davidson and Langley Research Center (page images at HathiTrust)
FREE-FLIGHT AERODYNAMIC-HEATING DATA TO MACH NUMBER 10.4 FOR A MODIFIED VON KARMAN NOSE SHAPE. (Defense Technical Information Center, 1961), by COLLIE,KATHERINE A, BLAND,WILLIAM M JR, and NATIONAL AERONAUTICS AND SPACE ADMINISTRATION WASHINGTON D C. (page images at HathiTrust; US access only)
An investigation of heat transfer within regions of separated flow at a Mach number of 6.0 (National Aeronautics and Space Administration ;, 1965), by Paul F. Holloway, Helen S. Creekmore, James R. Sterrett, and Langley Research Center (page images at HathiTrust)
Interference heating on a swept cylinder in region of intersection with a wedge at Mach number 8 (National Aeronautics and Space Administration ;, 1965), by Dennis M. Bushnell and Langley Research Center (page images at HathiTrust)
A study of methods for simulating the atmosphere entry of vehicles with small-scale models (National Aeronautics and Space Administration, 1960), by Byron L. Swenson and Ames Research Center (page images at HathiTrust)
Range of interface thermal conductance for aircraft joints (National Aeronautics and Space Administration, 1960), by Martin E. Barzelay and Syracuse University (page images at HathiTrust)
An approximate analysis of unsteady vaporization near the stagnation point of blunt bodies (National Aeronautics and Space Administration, 1959), by Leonard Roberts and Langley Research Center (page images at HathiTrust)
Theoretical analysis of the creep collapse of columns (National Aeronautics and Space Administration, 1959), by Floyd R. Schlechte and Langley Research Center (page images at HathiTrust)
Effect of chordwise heat conduction on the torsional stiffness of a diamond-shaped wing subjected to a constant heat input (National Aeronautics and Space Administration, 1959), by Robert G. Thomson, J. Lyell Sanders, and Langley Research Center (page images at HathiTrust)
An experimental and theoretical investigation of the pressure distribution and flow fields of blunted cones at hypersonic Mach number (National Aeronautics and Space Administration, 1965), by Joseph W. Cleary and United States National Aeronautics and Space Administration (page images at HathiTrust)
Free-flight investigation of heat transfer to an unswept cylinder subjected to an incident shock and flow interference from an upstream body at Mach numbers up to 5.50 (National Aeronautics and Space Administration, 1961), by Howard S. Carter, Robert E. Carr, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
Laminar heat-transfer distributions for a blunted-cone, cone-frustum reentry configuration at Mach 10 (National Aeronautics and Space Administration ;, 1969), by J. David Dearing and Langley Research Center (page images at HathiTrust)
NASA TN D-3486 (National Aeronautics and Space Administration :, 1966), by C. M. Pittman, William D. Brewer, and United States National Aeronautics and Space Administration (page images at HathiTrust)
NASA TN D-4114 (National Aeronautics and Space Administration ;, 1967), by Ernest V. Zoby, Casimir J. Jachimowski, Jane T. Kemper, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Curve fits of predicted inviscid stagnation-point radiative heating rates, cooling factors, and shock standoff distances for hyperbolic earth entry (National Aeronautics and Space Administration ;, 1974), by John T. Suttles, Stephen B. Margolis, Edward M. Sullivan, and Langley Research Center (page images at HathiTrust)
Safe atmosphere entry of an isotope heat source with a single stable trim attitude at hypersonic speeds (National Aeronautics and Space Administration ;, 1972), by Lionel L. Levy, Raymond K. Burns, and Ames Research Center (page images at HathiTrust)
Apollo experience report : aerothermodynamics evaluation (National Aeronautics and Space Administration ;, 1972), by Dorothy B. Lee and Manned Spacecraft Center (U.S.) (page images at HathiTrust)
Analytical and experimental studies of shock interference heating in hypersonic flows (National Aeronautics and Space Administration ;, 1973), by J. Wayne Keyes, Frank D. Hains, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
Aerodynamic heating and loading within large open cavities in cone and cone-cyclinder-flare models at Mach 6.7 (National Aeronautics and Space Administration ;, 1974), by L. Roane Hunt and Langley Research Center (page images at HathiTrust)
Heat-transfer and pressure distributions on hemisphere-cylinders in methane-air combustion products at Mach 7 (National Aeronautics and Space Administration ;, 1973), by Irving Weinstein, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
NASA TN D-6138 (National Aeronautics and Space Administration :, 1971), by James Campbell Robinson, George F. Klich, Robert R. McWithey, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
Effect of wing sweep, angle of attack, Reynolds number, and wing root fillet on the interference heating to the wing windward surface of an entry vehicle configuration (National Aeronautics and Space Administration ;, 1972), by Louis E. Clark, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
Experimental heat-transfer and friction coefficients for air flowing through stacks of parallel flat plates (NACA, 1954), by Eldon W. Sams, Walter F. Weiland, United States National Advisory Committee for Aeronautics, and Lewis Research Center (page images at HathiTrust)
An integral analysis of heat transfer downstream of a rearward-facing step with small coolant injection. (National Aeronautics and Space Administration; [for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va.], 1970), by Keiichi Karashima (page images at HathiTrust; US access only)
A comparative analysis of the performance of long-range hypervelocity vehicles (National Advisory Committee for Aeronautics, 1957), by Alfred J. Eggers, Stanford E. Neice, H. Julian Allen, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
Correlation of heat-transfer and friction data for air flowing in inconel tube with rounded entrance (National Advisory Committee for Aeronautics, 1949), by Warren H. Lowdermilk, Milton D. Grele, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
Heat transfer from high-temperature surfaces to fluids. [Part] 1, Preliminary investigation with air in inconel tube with rounded entrance, inside diameter of 0.4 inch and length of 24 inches (National Advisory Committee for Aeronautics, 1948), by Leroy V. Humble, Milton Grele, Warren H. Lowdermilk, United States National Advisory Committee for Aeronautics, and Flight Propulsion Research Laboratory (page images at HathiTrust)
A discussion of methods for reducing aerodynamic heating in supersonic flight (National Advisory Committee for Aeronautics, 1955), by A. J. Eggers and Ames Research Center (page images at HathiTrust)
Measurements of aerodynamic heating obtained during demonstration flight tests of the Douglas D-558-II airplane (National Advisory Committee for Aeronautics, 1952), by Ira P. Jones, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
Preliminary results of supersonic-jet tests of simplified wing structures (National Advisory Committee for Aeronautics, 1953), by Richard R. Heldenfels, Richard Rosecrans, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
Transient temperature distribution in an aerodynamically heated multiweb wing (National Advisory Committee for Aeronautics, 1953), by George E. Griffith, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
Aerodynamic-heating data obtained from free-flight tests between Mach numbers of 1 and 5 (National Advisory Committee for Aeronautics, 1955), by Charles B. Rumsey, Russell N. Hopko, Robert O. Piland, Langley Aeronautical Laboratory, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
Free-flight measurements of aerodynamic heat transfer to Mach number 3.9 and of drag to Mach number 6.9 of a fin-stabilized cone-cylinder configuration (National Advisory Committee for Aeronautics, 1955), by Charles B. Rumsey, Langley Aeronautical Laboratory, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
Flutter at very high speeds (National Advisory Committee for Aeronautics, 1957), by Harry L. Runyan, Homer G. Morgan, Langley Aeronautical Laboratory, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
Local heat transfer to blunt noses at high supersonic speeds (National Advisory Committee for Aeronautics, 1957), by William E. Stoney, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
Preliminary investigation of lithium hydride as a high-temperature internal coolant (National Advisory Committee for Aeronautics, 1957), by Jerry L. Modisette, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
Measurements of aerodynamic heat transfer in turbulent separated regions at a Mach number of 1.8 (National Advisory Committee for Aeronautics, 1958), by Benjamine J. Garland, J. R. Hall, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
Aerodynamic heating and the deflection of drops by an obstacle in an air stream in relation to aircraft icing (National Advisory Committee for Aeronautics, 1940), by Arthur Kantrowitz and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
The effect of nonuniform temperature distributions on the stresses and distortions of stiffened-shell structures (National Advisory Committee for Aeronautics, 1950), by Richard R. Heldenfels and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
The compressible laminar boundary layer with fluid injection (National Advisory Committee for Aeronautics, 1955), by George M. Low and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
Elevated-temperature tests under static and aerodynamic conditions on honeycomb-core sandwich panels (National Aeronautics and Space Administration, 1959), by Joseph M. Groen, Aldie E. Johnson, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Structures for reentry heating (National Aeronautics and Space Administration, 1961), by Roger A. Anderson, Robert T. Swann, and Langley Research Center (page images at HathiTrust; US access only)
Heat transfer to blunt axially symmetric bodies (National Aeronautics and Space Administration, 1960), by John O. Reller and Ames Research Center (page images at HathiTrust; US access only)
Elevated-temperature tests under static and aerodynamic conditions on corrugated-stiffened panels (National Aeronautics and Space Administration, 1959), by Joseph M. Groen, Richard Rosecrans, and United States National Aeronautics and Space Administration (page images at HathiTrust)
A comparison of stagnation-point heating in a rocket exhaust to that of actual flight ([Sandia Corp.], 1961), by Frank L. Paris (page images at HathiTrust; US access only)
Test of 61S-T6 aluminum sheet under short-duration, high rate of rise, heating (Sandia Corporation ;, 1958), by J. A. Barber and Sandia Corporation (page images at HathiTrust; US access only)
Calculation of surface temperatures in steady supersonic flight (National Advisory Committee for Aeronautics, 1946), by George P. Wood and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
Preliminary analysis of the capabilities of a composite slab for an advanced heat-sink design (Wright Air Development Division, Air Research and Development Command, U.S. Air Force, 1961), by Paul A. Libby (page images at HathiTrust)
Gas dynamics in space exploration ; [scientific papers] (National Aeronautics and Space Administration, Office of Scientific and Technical Information ; [for sale by the Superintendent of Documents, U.S.Govt. Print.Off.], 1963), by Chicago NASA-University Conference on the Science and Technology of Space Exploration (page images at HathiTrust)
Distribution of ROBIN sensed wind shears at 30 to 70 kilometers (L.G. Hanscom Field, Bedford, Massachusetts : Air Force Cambridge Research Laboratories, Office of Aerospace Research, United States Air Force, 1969., 1969), by Henry A. Salmela, Norman Sissenwine, and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
Experimental investigation of the simulation of atmospheric entry of ballistic missiles (National Advisory Committee for Aeronautics, 1957), by Stanford E. Neice, Bernard E. Cunningham, James A. Carson, Ames Laboratory, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
Horizontal scale variations in satellite estimates of weather erosion parameters for reentry systems (Hanscom AFB, Massachusetts : Air Force Geophysics Laboratory, Air Force Systems Command, United States Air Force, 1980., 1980), by James T. Bunting, C. N. Touart, and U.S. Air Force Geophysics Laboratory (page images at HathiTrust)
Methods for conducting short-time tensile, creep, and creep-rupture tests under conditions of rapid heating (Columbus, Ohio : Defense Metals Information Center, Battelle Memorial Institute, 1959., 1959), by Donald P. Moon, Ward F. Simmons, Defense Metals Information Center (U.S.), and United States. Office of the Director of Defense Research and Engineering (page images at HathiTrust)
Selected short-time tensile and creep data obtained under conditions of rapid hearting (Columbus, Ohio : Defense Metals Information Center, Battelle Memorial Institute, 1959., 1960), by Donald P. Moon, Ward F. Simmons, Defense Metals Information Center (U.S.), and United States. Office of the Director of Defense Research and Engineering (page images at HathiTrust)
Charts of equilibrium real-gas stagnation point conditions on a sphere for altitudes to 200,000 feet and velocities to 15,000 feet per second (White Oak, Maryland : United States Naval Ordnance Laboratory, 1964., 1964), by P. D. Fisher and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
Use of phase-change paints to study fin-body interference heating (Silver Spring, Maryland : Naval Surface Weapons Center, White Oak Laboratory, 1976., 1976), by Jr. Gillerlain and Naval Surface Weapons Center. : White Oak Laboratory (page images at HathiTrust)
Normal impingement of a supersonic jet on a plane : a basic study of shock-interference heating (Silver Spring, Maryland : Naval Surface Weapons Center, White Oak Laboratory, 1975., 1975), by Kuei-Yuan Chien and Naval Surface Weapons Center. White Oak Laboratory (page images at HathiTrust)
Interacting supersonic turbulent boundary layers over a two-dimensional protuberance. (Silver Spring, Maryland : Naval Ordnance Laboratory, White Oak, 1974., 1974), by Arnold Polak and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
Experimental investigation of a fin-cone interference flow field at Mach 5 (Silver Spring, Maryland : Naval Surface Weapons Center, 1976., 1976), by Jr. Gillerlain and Naval Surface Weapons Center. White Oak Laboratory (page images at HathiTrust)
an Integral approach to transient heat-conduction problems with phase transition (Silver Spring, Maryland : Naval Surface Weapons Center, White Oak Laboratory, 1975., 1975), by Tse-Fou Zien and Naval Surface Weapons Center. White Oak Laboratory (page images at HathiTrust)
Boundary-layer transition experiments on pre-ablated graphite nosetips in a hyperballistics range (Silver Spring, Maryland : Naval Surface Weapons Center, White Oak Laboratory, 1976., 1976), by Daniel C. Reda, Robert A. Leverance, and Naval Surface Weapons Center. White Oak Laboratory (page images at HathiTrust)
Heat transfer and frictional effects in laminar boundary layers : Part 5. The modified Lighthill Method for determining the rate of heat transfer (Wright-Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1954, 1954), by Arthur N. Tifford, United States. Air Force. Air Research and Development Command, Wright Air Development Center, and Ohio State University. Research Foundation (page images at HathiTrust)
Procedures for including temperature effects in structural analyses of elastic wings - part I an equivalent plate method of structural analysis for elevated temperature structures (Wright Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1958., 1958), by William R. Mills, United States. Air Force. Air Research and Development Command, and Wright Air Development Center (page images at HathiTrust)
Elasto-plastic analysis of structures under load and two-dimensional temperature distributions. Volume 1, Analysis development and experimental program (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1962., 1962), by P. C. Huang, R. J. Edwards, United States. Air Force. Systems Command. Aeronautical Systems Division, Air Force Flight Dynamics Laboratory (U.S.), and Martin Marietta Corporation. Baltimore Division (page images at HathiTrust)
Induction heating and theory in the solution of transient problems of aircraft structures (Wright-Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Center, United States Air Force 1956., 1956), by N. J. Hoff, Burton Erickson, V. Wagle, S. Lederman, I. Mirsky, Irwin Berman, Frederick Pohle, United States. Air Force. Air Research and Development Command, Wright Air Development Center, and Polytechnic Institute of Brooklyn. Department of Aeronautical Engineering and Applied Mechanics (page images at HathiTrust)
Aerodynamic heating and heat transfer for airfoils at Mach numbers of 2.74 through 5.7 (Wright-Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1955., 1955), by A. E. Abramson, J. A. Zdrazil, W. L. Torgeson, United States. Air Force. Air Research and Development Command, Wright Air Development Center, and Inc Research (page images at HathiTrust)
An experimental study of the distribution of convective heat transfer to a large-scale model of parachute cloth (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1966., 1966), by E. R. G. Eckert, K. M. Krall, C. J. Scott, M. Ruiz-Urbieta, J. E. Anderson, Wright-Patterson Air Force Base (Ohio), University of Minnesota, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
Thermal effects on static aeroelastic stability and control : description and results of tests conducted to determine the thermally affected deflectional behavior of corrugated multiweb wing structures (Wright-Patterson Air Force Base, Ohio : Wright Air Development Division, Aeromechanics Branch, Air Research and Development Command, United States Air Force, 1959., 1959), by James F. Quinn, Richard H. Gallagher, Donald Turrentine, Bell Aircraft Corporation, United States. Wright Air Development Division, and United States. Air Force. Air Research and Development Command (page images at HathiTrust)
Pressure and heat transfer measurements for hypersonic flows over expansion corners and ahead of ramps (Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, 1963), by Louis G. Kaufman, Air Force Flight Dynamics Laboratory (U.S.), United States. Air Force. Systems Command. Aeronautical Systems Division, and Grumman Aircraft Engineering Corporation. Research Department (page images at HathiTrust)
Heat barrier coatings (Wright-Patterson Air Force Base, Ohio : Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1961., 1961), by Buford A. Macklin, Elihu A. Schatz, James C. Withers, United States. Air Force. Systems Command. Aeronautical Systems Division, and United States. Air Force. Systems Command. Aeronautical Systems Division. Directorate of Materials and Processesd States (page images at HathiTrust)
Theory and experiment in the solution of structural problems of supersonic aircraft (Wright-Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1956., 1956), by Nicholas J. Hoff, Lederman,S., MacLean,William R., Alexander Chwick, William I. Berks, I. Mirsky, Henry Oliver, Frederick V. Pohle, Martin Bloom, Wright Air Development Center, and Polytechnic Institute of Brooklyn (page images at HathiTrust)
Aerodynamic applications of plasma wind tunnels (Wright-Patterson Air Force Base, Ohio : Aeronautical Research Laboratory, Wright Air Development Division, Air Research and Development Command, United States Air Force, 1960., 1960), by Jackson R. Stalder, Boris Ragent, Charles E. Noble, Frederick K. Goodwin, United States. Air Force. Air Research and Development Command, and United States. Wright Air Development Center (page images at HathiTrust)
Laminar heat transfer on blunt-nosed bodies in three-dimensional hypersonic flow (Wright-Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1958., 1958), by Roberto Vaglio-Laurin, United States. Air Force. Air Research and Development Command, Wright Air Development Center, and Polytechnic Institute of Brooklyn. Department of Aeronautical Engineering and Applied Mechanics (page images at HathiTrust)
Proceedings of Symposium on Aerothermoelasticity ; 30-31 October and 1 November 1961 (Wright-Patterson Air Force Base, Ohio : Aeronautical Systems Division, Air Force Systems Command, United States Air Force, [1962], 1962), by David M. Jones and United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
Evaluation of several hypersonic turbulent heat transfer analyses by comparison with experimental data (Wright-Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research Development and Command, United States Air Force, 1957., 1957), by Paul A. Libby, Robert J. Cresci, United States. Air Force. Air Research and Development Command, Wright Air Development Center, and Polytechnic Institute of Brooklyn. |b Department of Aerospace Engineering and Applied Mechanics (page images at HathiTrust)
High speed flow and aerodynamic heating behavior of porous fibrous structures (Wright-Patterson Air Force Base, Ohio : Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1961., 1961), by Myron J. Coplan, United States. Air Force. Systems Command, and United States. Air Force. Systems Command. Aeronautical Systems Division. Directorate of Materials and Processes (page images at HathiTrust)
Two-dimensional supersonic nonadiabatic flow and axisymmetric supersonic adiabatic and nonadiabatic flows (Wright-Patterson Air Force Base, Ohio : b Air Force Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, 1966., 1966), by Jack Norman Nielsen, Frederick K. Goodwin, Larry L. Lynes, Wright-Patterson Air Force Base (Ohio), Itek Corporation, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
Elasto-plastic analysis of structures under load and two-dimensional temperature distributions. Volume 2, Summary of test data (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1962., 1962), by P. C. Huang, R. J. Edwards, United States. Air Force. Systems Command. Aeronautical Systems Division, Air Force Flight Dynamics Laboratory (U.S.), and Martin Marietta Corporation. Baltimore Division (page images at HathiTrust)
The analytical determination of the thermal response of a typical aircraft structure subjected to transient external heating and cooling (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1966., 1966), by Thomas N. Bernstein, Robert M. Engle, Gene E. Maddux, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
Laminar heat transfer on sharp and blunt ten-degree cones in conical and parallel low-density flow (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1973., 1973), by David E. Boylan, Inc ARO, Arnold Engineering Development Center, and United States. Air Force. Systems Command (page images at HathiTrust)
Shock wave - turbulent boundary layer interaction in high speed flow (Wright-Patterson Air Force Base, Ohio : Aerospace Research Laboratories, Air Force Systems Command, United States Air Force, 1975., 1975), by Michael S. Holden, Aerospace Research Laboratories (U.S.), and Calspan Corporation (page images at HathiTrust)
Free flight hypersonic heat transfer and boundary layer transition studies: HTV flights A-40 and A-41 (Wright-Patterson Air Force Base, Ohio : Aeronautical Research Laboratories, Air Force Research Division, Air Research and Development Command, United States Air Force, 1960., 1960), by James E. Brunk, Warren N. White, Aerospace Research Laboratories (U.S.), and Curtiss-Wright Corporation (page images at HathiTrust)
An investigation of the half-model reflection-plane technique for dynamic stability testing at transonic Mach numbers (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1977., 1977), by T. O. Shadow, United States. Air Force. Systems Command, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
Ablation modeling for dynamic simulation of reentry vehicles : preprint (Wright Patterson Air Force Base, Ohio : Air Vehicles Directorte, Air Force Research Laboratory, Air Force Materiel Command, 2006., 2006), by David B. Doman, William B. Blake, and Ohio). Air Vehicles Directorate Air Force Research Laboratory (Wright-Patterson Air Force Base (page images at HathiTrust)
Aerodynamic heating and heat transfer phenomena at Mach numbers 3 to 4 (Wright-Patterson Air Force Base, Ohio : Wright Air Development Center, Equipment Laboratory, Air Research and Development Command, United States Air Force, 1951., 1951), by K. G. Anderson, J. M. Durben, H. B. Merrell, Wright Air Development Center, and United States. Air Force. Air Research and Development Command (page images at HathiTrust)
Low-density stagnation-point heat transfer in hypersonic air flow (Wright-Patterson Air Force Base, Ohio : Aeronautical Research Laboratory, Air Force Research Division, Air Research and Development Command, United States Air Force, 1961., 1961), by Charles F. Wittliff, Merle R. Wilson, Aerospace Research Laboratories (U.S.), and Cornell Aeronautical Laboratory (page images at HathiTrust)
Real gas scale effects on hypersonic laminar boundary-layer parameters including effects of entropy-layer swallowing (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1975., 1975), by J. C. Adams, E. O. Marchand, A. W. Mayne, W. R. Martindale, United States. Air Force. Arnold Air Force Base, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
Three-dimensional shock wave-turbulent boundary layer interactions at Mach 6 (Wright-Patterson Air Force Base, Ohio : Aerospace Research Laboratories, Air Force Systems Command, United States Air Force, 1975., 1975), by C. Herbert Law and Aerospace Research Laboratories (U.S.) (page images at HathiTrust)
Development of test facilities for studies in hypersonic range. Part II (Wright-Patterson Air Force Base, Ohio : Wright Air Development Division, Air Research and Development Command, United States Air Force, 1960., 1960), by Henry Halle, Channon F. Price, United States. Air Force. Air Research and Development Command, United States. Wright Air Development Division, and University of Chicago (page images at HathiTrust)
Thermo-structural analysis manual. Volume I (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Directorate of Materials and Processes, Aeronautical Systems Division, Air Force Systems Command, U.S. Air Force, 1962., 1962), by H. Switzky, M. Noiman, Marvin J. Forray, United States. Air Force. Systems Command. Aeronautical Systems Division. Directorate of Materials and Processes, and Republic Aviation Corporation (page images at HathiTrust)
Development of test facilities for studies in hypersonic range. Part I (Wright-Patterson Air Force Base, Ohio : Wright Air Development Division, Air Research and Development Command, United States Air Force, 1960., 1960), by Henry Halle, Channon F. Price, United States. Air Force. Air Research and Development Command, United States. Wright Air Development Division, and University of Chicago (page images at HathiTrust)
Applied heat transfer course lecture notes on interference flows (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Flight Mechanics Division, High Speed Aero Performance Branch, Air Force Systems Command, United States Air Force, 1972., 1972), by Gerald L. Burke and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
A design manual for determining the thermal characteristics of high speed aircraft (Wright Field, Dayton, Ohio : Army Air Forces, Materiel Command, 1938., 1947), by H. A. Johnson, L. Possner, E. G. Slack, F. M. Sauer, Morris W. Rubesin, Berkeley. Department of Mechanical Engineering University of California, and United States. Army Air Forces. Air Matériel Command (page images at HathiTrust)
An Analytical study of the use of air-equivalent hot gaseous mixtures for aerodynamic test purposes (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Research and Development Command, United States Air Force, 1959., 1959), by Kenneth E. Tempelmeyer, Inc ARO, Arnold Engineering Development Center, and United States. Air Force. Air Research and Development Command (page images at HathiTrust)
Laminar, transitional, and turbulent heat transfer measurements on a yawed blunt conical nosetip (Los Angeles, California : Space and Missile Systems Organization, Los Angeles Air Force Station, Air Force Systems Command, United States Air Force, 1972., 1972), by George F. Widhopf, United States. Air Force. Systems Command, Space and Missile Systems Organization (U.S.), and Aerospace Corporation (page images at HathiTrust)
Analytical and experimental thermal analysis of a guided bomb (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1981., 1981), by W. K. Crain, R. K. Matthews, Inc ARO, Arnold Engineering Development Center, and United States. Air Force. Systems Command (page images at HathiTrust)
Heat transfer and temperature distribution in a hemispherical nose cone in hypersonic flow (Polytechnic Institute of Brooklyn, Department of Aerospace Engineering and Applied Mechanics, 1962), by S. V. Nardo, Ronald W. Sadler, and Polytechnic Institute of Brooklyn. Dept. of Aerospace Engineering and Applied Mechanics (page images at HathiTrust)
Experimental heat transfer and temperature distribution in a hollow tube with internal airflow at high temperature and pressure (Polytechnic Institute of Brooklyn, Department of Aerospace Engineering and Applied Mechanics, 1962), by S. V. Nardo, Lawrence D. Brown, and Polytechnic Institute of Brooklyn. Dept. of Aerospace Engineering and Applied Mechanics (page images at HathiTrust)
Acoustic receptivity of compressible boundary layers : receptivity via surface-temperature variations (National Aeronautics and Space Administration, Langley Research Center ;, 1994), by Meelan Choudhari and Langley Research Center (page images at HathiTrust)
A review and development of correlations for base pressure and base heating in supersonic flow (Albuquerque, New Mexico : Sandia National Laboratories, Aerodynamics Department, 1993., 1993), by J. Parker Lamb, William L. Oberkampf, United States. Department of Energy, University of Texas at Austin. Department of Mechanical Engineering, and Sandia National Laboratories (page images at HathiTrust)
Procedures for the design of thermal protection systems for maneuverable re-entry vehicles (Wright-Patterson Air Force Base, Ohio : Booster and Power Division, Dyna-Soar Enginering Office, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1962., 1962), by Donald Turrentine and United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
Boundary-layer trip effectiveness and computations of aerodynamic heating for XM797 nose-tip configurations (Aberdeen Proving Ground, Maryland : Ballistic Research Laboratory, 1983., 1983), by Walter B. Sturek, Donald C. Mylin, Lyle D. Kayser, and U.S. Army Ballistic Research Laboratory (page images at HathiTrust)
Supersonic aerodynamic heat transfer and pressure distributions on a sphere-cone model at high angles of yaw (White Oak, Maryland : United States Naval Ordance Laboratory, 1962., 1962), by Lionel Pasiuk and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
Computational study of swept-fin aerodynamic heating for the 105mm M774 (Aberdeen Proving Ground, Maryland : Ballistic Research Laboratory, 1983., 1983), by Walter B. Sturek, Paul Weinacht, Lyle D. Kayser, and U.S. Army Ballistic Research Laboratory (page images at HathiTrust)
Constant-Mach-number simulation of critical flight loads on high-velocity projectile fuzes (Washington, D.C.: U.S. Army Material Command, Harry Diamond Laboratories, 1969., 1969), by Frank T. Buckley and U.S. Army Harry Diamond Laboratories (page images at HathiTrust)
Computational study of inbore and inflight heating for the 105MM, M774 projectile modified swept fin (Aberdeen Proving Ground, Maryland : Ballistic Research Laboratory, 1984., 1984), by Paul Weinacht, Perry A. Wooden, Walter B. Sturek, and U.S. Army Ballistic Research Laboratory (page images at HathiTrust)
Improved aeroprediction code. Part II, Computer program user's guide and listing (Dahlgren, Virginia : Weapons Systems Department, Naval Surface Warfare Center, Dahlgren Division, 1993., 1993), by Frank G. Moore, Thomas C. Hymer, Roy Mitchell McInville, and Naval Surface Warfare Center (U.S.). Dahlgren Division (page images at HathiTrust)
Improved aeroprediction code. Part I, Summary of new methods and comparison with experiment (Dahlgren, Virginia : Weapons Systems Department, Naval Surface Warfare Center, Dahlgren Division, 1993., 1993), by Frank G. Moore, Roy Mitchell McInville, Thomas C. Hymer, and Naval Surface Warfare Center (U.S.). Dahlgren Division (page images at HathiTrust)
Computational modeling of aerodynamic heating for XM797 nose cap configurations (Aberdeen Proving Ground, Maryland : U.S. Army Armament Research and Development Command, Ballistic Research Laboratory, 1983., 1983), by Walter B. Sturek, Henry Hudgins, Donald C. Mylin, Lyle D. Kayser, U.S. Army Ballistic Research Laboratory, and United States. Army Armament Research and Development Command (page images at HathiTrust)
Supersonic/hypersonic aerodynamics and heat transfer for projectile design Using viscous-inviscid interaction (Aberdeen Proving Ground, Maryland : U.S. Army Ballistic Research Laboratory, 1990., 1990), by Michael J. Nusca and U.S. Army Ballistic Research Laboratory (page images at HathiTrust)
Aerodynamic heating of ordnance projectiles (Adelphi, Maryland : U.S. Army Material Command, Harry Diamond Laboratories, 1975., 1975), by Harry J. Davis, K. Jeanne Achstetter, and U.S. Army Harry Diamond Laboratories (page images at HathiTrust)
Experiments on the thermal performance of ribbon parachutes (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1965., 1965), by C. J. Scott, E. R. G. Eckert, United States. Air Force. Systems Command. Research and Technology Division, Air Force Flight Dynamics Laboratory (U.S.), and University of Minnesota. Department of Mechanical Engineering (page images at HathiTrust)

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