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Aerothermodynamics

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• Aerodynamics, Supersonic
• Aerodynamics, Transonic
• Astronautics
• High-speed aeronautics
• Thermodynamics

• Ablation (Aerothermodynamics)
• Aerodynamic heating
• Artificial satellites -- Atmospheric entry
• Plasma sheaths

• Thermoaerodynamics

• Heat-transfer and pressure distributions at Mach numbers of 6.0 and 9.6 over two reentry configurations for the five-stage scout vehicle / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1963), by Paul F. Holloway, James C. Dunavant, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Radiative heating of vehicles entering the earth's atmosphere / (Washington : National Aeronautics and Space Administration, 1962), by Bradford H. Wick and North Atlantic Treaty Organization. Advisory Group for Aeronautical Research and Development (page images at HathiTrust)
• Probabilistic modeling for simulation of aerodynamic uncertainties in propulsion systems ([Washington, D.C.] : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1989]), by A. Hamed, United States National Aeronautics and Space Administration, and Lewis Research Center. Institute for Computational Mechanics in Propulsion (page images at HathiTrust)
• Table and charts of equilibrium normal shock and shock-tube properties for pure argon with velocities to 18 km/sec / (Washington : Scientific and Technical Information Office, National Aeronautics and Space Administration ; Springfield, Va. : for sale by the National Technical Information Service, 1976), by Charles G. Miller, Sue E. Wilder, and Langley Research Center (page images at HathiTrust)
• Supersonic free-flight measurements of heat transfer and transition on a 10° cone having a low temperature ratio / (Washington, [D.C.] : National Aeronautical and Space Administration, 1961), by Charles F. Merlet, Charles B. Rumsey, United States National Aeronautics and Space Administration, and Langley Research Center (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 / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1990), by William L. Wells and Langley Research Center (page images at HathiTrust)
• NASA Aerodynamics Program : annual report 1990 / ([Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991), by Louis J. Williams and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program (page images at HathiTrust)
• A study for development of aerothermodynamic test model materials and fabrication technique / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1972), by W. G. Dean, L. E. Connor, Langley Research Center, and Lockheed Missiles and Space Company (page images at HathiTrust)
• Aerothermal performance and structural integrity of a René 41 thermal protection system at Mach 6.6 / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by William D. Deveikis and Langley Research Center (page images at HathiTrust)
• Apollo experience report : spacecraft heating environment and thermal protection for launch through the atmosphere of the earth / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by Robert L. Dotts and Manned Spacecraft Center (U.S.) (page images at HathiTrust)
• Aerodynamic heating of conical entry vehicles at speeds in excess of earth parabolic speed / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, VA] : National Technical Information Service, distributor, 1963), by H. Jullian Allen, United States National Aeronautics and Space Administration, and Ames Research Center (page images at HathiTrust)
• Effect of interplanetary trajectory options on a manned Mars aerobrake configuration / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1990), by Robert D. Braun, Lin C. Hartung, Richard W. Powell, and Langley Research Center (page images at HathiTrust)
• Numerical studies of convective cooling for a locally heated skin / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1991), by Stephen J. Scotti and Langley Research Center (page images at HathiTrust)
• Heat-transfer and pressure distributions for laminar separated flows downstream of rearward-facing steps with and without mass suction / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Ronald D. Brown, Antoni K. Jakubowski, and Langley Research Center (page images at HathiTrust)
• Apollo experience report : aerothermodynamics evaluation / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1972), by Dorothy B. Lee and Manned Spacecraft Center (U.S.) (page images at HathiTrust)
• The aerothermodynamic environment of the Apollo command module during suborbital entry / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1972), by Dorothy B. Lee, Winston D. Goodrich, and Manned Spacecraft Center (U.S.) (page images at HathiTrust)
• Hypersonic aerodynamics and entry-maneuver--aerothermodynamic interactions for two lifting entry vehicles / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1972), by James P. Arrington, William C. Woods, and Langley Research Center (page images at HathiTrust)
• Thermal buckling of solid wings. ([Brooklyn] Polytechnic Institute of Brooklyn, Dept. of Aeronatical Engineering and Applied Mechanics, 1957), by Josef Singer (page images at HathiTrust)
• Table and charts of equilibrium normal-shock and shock-tube properties for pure carbon dioxide with velocities from 1 to 16 km/sec / (Washington : Scientific and Technical Information Office, National Aeronautics and Space Administration ; Springfield, Va. : for sale by the National Technical Information Service, 1976), by Charles G. Miller, Sue E. Wilder, and Langley Research Center (page images at HathiTrust)
• The Aerothermodynamics of aircraft gas turbine engines / (Wright-Patterson AFB, Ohio : Air Force Aero Propulsion Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command ; Washington : U.S. Govt. Print. Off., 1978), by Gordon C. Oates, Air Force Aero Propulsion Laboratory (U.S.), and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
• Aerothermodynamic consequences of nozzle nonequilibrium ([Arnold Air Force Station, Tenn., Arnold Engineering Development Center, Air Force Systems Command, 1966]), by A. F. Burke and J. E. Wallace (page images at HathiTrust)
• Transport coefficients of air to 8000° K / (Wilmington, Mass. : Research and Advanced Development Division, Avco Manufacturing Corporation, 1958), by Ernest Bauer, Martin Zlotnick, and Avco Corporation. Research and Advanced Development Division (page images at HathiTrust)
• Axisymmetric Hall-arc jet wind tunnel driver study ([Wright-Patterson Air Force Base, Ohio, Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, 1967]), by Robert Richter, Rolf D. Buhler, and Peter Lenn (page images at HathiTrust)
• Computer program for one-dimensional nonequilibrium reacting gas flow ([Wright-Patterson Air Force Base, Ohio, Air Force Flight Dynamics Laboratory, Directorate of Laboratories, Air Force Systems Command, 1967]), by H. S. Dresser, H. G. Webb, and E. P. French (page images at HathiTrust)
• Proceedings. [David M. Jones, Symposium chairman] (Wright-Patterson Air Force Base, Ohio : Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1962), by Ohio) Symposium on Aerothermoelasticity (1st : 1961 : Dayton, David M. Jones, and United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust; US access only)
• Thermodynamics of chemical species important to rocket technology. ([Washington] U.S. Dept. of Commerce, National Bureau of Standards, 1973), by Thomas B. Douglas, Charles W. Beckett, United States. National Bureau of Standards. Physical Chemistry Division, and United States. National Bureau of Standards (page images at HathiTrust)
• Effects of flow separation and cove leakage on pressure and heat-transfer distributions along a wing-cove-elevon configuration at Mach 6.9 / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1983), by William D. Deveikis and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Aerothermal tests of quilted dome models on a flat plate at a Mach number of 6.5 / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1988), by Christopher E. Glass, L. Roane Hunt, and Langley Research Center (page images at HathiTrust)
• OAST space technology accomplishments FY 1991 / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : For sale by the National Technical Information Service], 1992), by United States. Office of Aeronautics and Space Technology and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program (page images at HathiTrust)
• Computational method to predict thermodynamic, transport, and flow properties for the modified Langley 8-foot high-temperature tunnel / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by S. Venkateswaran, Ramadas K. Prabhu, L. Roane Hunt, and Langley Research Center (page images at HathiTrust)
• An Inlet analysis for the NASA hypersonic research engine aerothermodynamic integration model / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Earl H. Andrews and Langley Research Center (page images at HathiTrust)
• Aerothermal evaluation of a spherically blunted body with a trapezoidal cross section in the Langley 8-foot high-temperature tunnel / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1986), by Cindy W. Albertson 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 / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1986), by Christopher E. Glass, L. Roane Hunt, and Langley Research Center (page images at HathiTrust)
• Preliminary analysis of remote infrared imagery of shuttle during entry : an aerothermodynamic flight experiment / (Washington : National Aeronautics and Space Administration, Scientific and Technical Information Service, 1977), by Byron L. Swenson, Larry E. Edsinger, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Slip-boundary equations for multicomponent nonequilibrium airflow / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1985), by Roop N. Gupta, James N. Moss, Carl D. Scott, and Langley Research Center (page images at HathiTrust)
• Experimental and theoretical deposition rates from salt-seeded combustion gases of a Mach 0.3 burner rig / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1984), by Gilbert J. Santoro and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Experimental and predicted heating distributions for biconics at incidence in air at Mach 10 / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1984), by Charles G. Miller and Langley Research Center (page images at HathiTrust)
• Aerothermal environment in chordwise gaps between split elevons at Mach 6.8 / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1980), by L. Roane Hunt, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Wind-tunnel measurements and comparison with flight of the boundary layer and heat transfer on a hollow cylinder at Mach 3 / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1980), by Robert L. Stallings, Milton Lamb, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Analytical comparison of hypersonic flight and wind tunnel viscous/inviscid flow fields / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1975]), by H. J. Fivel, L. J. Mockapetris, R. V. Masek, Langley Research Center, and McDonnell Douglas Astronautics Company-East (page images at HathiTrust)
• Modulated entry / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [1960]), by Frederick C. Grant and Langley Research Center (page images at HathiTrust)
• Methods of predicting laminar heat rates on hypersonic vehicles / (Washington : National Aeronautics and Space Administration, [1959]), by Richard J. Wisniewski and Lewis Research Center (page images at HathiTrust)
• A simplified study on the nonequilibrium Couette and boundary-layer flows with air injection / (Washington : National Aeronautics and Space Administration, [1960]), by Paul M. Chung and Ames Research Center (page images at HathiTrust)
• A visual technique for determining qualitative aerodynamic heating rates on complex configurations / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [1960]), by P. Calvin Stainback and Langley Research Center (page images at HathiTrust)
• Steady internal flow and aerodynamic loads analysis of shuttle thermal protection system / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1984), by D. H. Petley and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Aerothermal tests of a 12.5⁰ cone at Mach 6.7 for various Reynolds numbers, angles of attack, and nose shapes / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1985), by Robert J. Nowak, L. Roane Hunt, Cindy W. Albertson, and Langley Research Center (page images at HathiTrust)
• Aerothermal analysis of a wing-elevon cove with variable leakage / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1980), by L. Roane Hunt, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Aerodynamic analysis of tektites and their parent bodies / (Washington, D.C. : National Aeronautics and Space Administration, 1962), by E. W. Adams and R. M. Huffaker (page images at HathiTrust)
• Shock interference heat transfer to tank configurations mated to a straight-wing space shuttle orbiter at mach number 10.3 / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1976), by Davis H. Crawford, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Aerothermal and structural performance of a cobalt-base superalloy thermal protection system at Mach 6.6 / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1977), by James Wayne Sawyer, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Unsteady stagnation-point heat transfer / (Washington : National Aeronautics and Space Administration, [1959]), by E. M. Sparrow and Lewis Research Center (page images at HathiTrust)
• 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 [electronic resource] / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1972), by Louis E. Clark, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Approximate thermodynamic, transport and electrical properties of high-temperature air. (Seattle, Boeing Co., 1963.), by R. J. Arave and Boeing Company (page images at HathiTrust; US access only)
• Transient reactor aerothermodynamics /, by Howard C. Rodean and Lawrence Radiation Laboratory (page images at HathiTrust)
• Supersonic flutter analyses including aerodynamic heating effects /, by R. L. Harder, United States. Air Force. Air Research and Development Command. sponsor, Wright Air Development Center issuing body, and Pasadena California Institute of Technology (page images at HathiTrust)
• Use of fusible temperature indicators for obtaining quantitative aerodynamic heat-transfer data, (Washington, D.C., U.S. National Aeronautics and Space Administration, 1966), by Robert A. Jones and James L. Hunt (page images at HathiTrust; US access only)
• Heat transfer from high-temperature surfaces to fluids. (Washington, [D.C.] : National Advisory Committee for Aeronautics, [1949]), by Warren H. Lowdermilk, Milton D. Grele, United States. National Advisory Committee for Aeronautics. NACA research memorandum, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Heat transfer from high-temperature surfaces to fluids. (Washington, [D.C.] : National Advisory Committee for Aeronautics, [1948]), by Leroy V. Humble, Milton Grele, Warren H. Lowdermilk, United States. National Advisory Committee for Aeronautics. NACA research memorandum, United States. National Advisory Committee for Aeronautics, and Flight Propulsion Research Laboratory (page images at HathiTrust)
• Measurements of aerodynamic heating obtained during demonstration flight tests of the Douglas D-558-II airplane / (Washington, D.C. : National Advisory Committee for Aeronautics, 1952), by Ira P. Jones, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
• Subsurface, surface, and boundary layer interactions of various transpirants with carbon /, by Thomas J. Dahm, U.S. Atomic Energy Commission, Aerotherm Corporation, and Sandia Corporation (page images at HathiTrust)
• Inverse-method and method-of-characteristics flow-field programs /, by J. B. Moreno, U.S. Atomic Energy Commission, and Sandia Corporation (page images at HathiTrust)
• Experimental investigation of a fin-cone interference flow field at Mach 5 /, by Jr. Gillerlain 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 /, by Daniel C Reda, Robert A. Leverance, and Naval Surface Weapons Center. White Oak Laboratory (page images at HathiTrust)
• Tables and charts of equilibrium thermodynamic properties of carbon dioxide for temperatures from 100 K to 25 000 K / (Washington, D. C. : Scientific and Technical Information Office, National Aeronautics and Space Administration ; Springfield, Va. : for sale by the National Technical Information Service, 1976), by Charles G. Miller, Sue E. Wilder, and Langley Research Center (page images at HathiTrust)
• Preliminary design and experimental investigation of the FDL-5A unmanned high L/D spacecraft.., by F. L. Guard, H. D. Schultz, issuing agency Air Force Flight Dynamics Laboratory (U.S.), and sponsor Lockheed-California Company (page images at HathiTrust)
• A short study of viscous constant-density aerodynamic equations in two-dimensional rectilinear coordinates / ([Albuquerque, N.M.] : Sandia Corporation, 1961), by W. B. Brooks and Sandia Corporation (page images at HathiTrust; US access only)
• An index of tables and charts for use in gas dynamic studies / (Albuquerque, New Mexico : Sandia Corporation, Technical Information Division ; Washington, D.C. : Available from the Office of Technical Services, Dept. of Commerce, [1961]), by D. E. Randall, U.S. Atomic Energy Commission, and Sandia Corporation (page images at HathiTrust)
• Special materials tests for the hypersonic plasma generator / (Albuquerque, New Mexico : [Sandia Corporpation], 1965), by K. J. Touryan (page images at HathiTrust; US access only)
• Heat-transfer and flow-field tests of the McDonnell Douglas-Martin Marietta space shuttle configurations /, by R. K. Matthews, R. H. Eaves, W. R. Martindale, sponsor Martin Marietta Corporation, sponsor McDonnell Douglas Corporation, Arnold Engineering Development Center. sponsor, United States. Air Force. Systems Command. issuing body, and Inc. ARO (page images at HathiTrust)
• Heat-transfer and flow-field tests of the North American Rockwell/ General Dynamics Convair space shuttle configurations /, by W. R. Martindale, L. L. Trimmer, R. K. Matthews, sponsor North American Rockwell Corporation, sponsor General Dynamics Corporation. Convair Division, Arnold Engineering Development Center. sponsor, United States. Air Force. Systems Command. issuing body, and Inc. ARO (page images at HathiTrust)
• Laminar, transitional, and turbulent heat transfer measurements on a yawed blunt conical nosetip /, by George F. Widhopf, issuing body United States. Air Force. Systems Command, sponsor Space and Missile Systems Organization (U.S.), and sponsor Aerospace Corporation (page images at HathiTrust)

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