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Shielding (Heat) -- Computer programs

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• Shielding (Heat)
• Computer programs

• CAVE : a computer code for two-dimensional transient heating analysis of conceptual thermal protection systems for hypersonic vehicles (National Aeronautics and Space Administration :, 1977), by Kenneth A. Rathjen and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)

Items below (if any) are from related and broader terms.

• 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)
• Structural performance of two aerobrake hexagonal heat shield panel concepts (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by John T. Dorsey, James W. Dyess, and Langley Research Center (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)
• Oxidation and emittance of superalloys in heat shield applications (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), by Karl E. Wiedemann, Jalaiah Unnam, Ronald K. Clark, and Langley Research Center (page images at HathiTrust)
• Evaluation of three thermal protection systems in a hypersonic high-heating-rate environment induces by an elevon deflected 30/̊ (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1977), by Allan H. Taylor, Irving Weinstein, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Experimental assessment of a computer program used in space shuttle orbiter entry heating analyses (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), by William L. Wells, JoAnn Hudgins, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
• Reinforced carbon-carbon oxidation behavior in convective and radiative environments (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by Donald M. Curry, Emily W. Stephens, K. J. Johansen, Vought Corporation, Lyndon B. Johnson Space Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Wind tunnel investigation of simulated helicopter engine exhaust interacting with windstream (National Aeronautics and Space Administration ;, 1974), by Craig S. Shaw, John C. Wilson, and Langley Research Center (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)
• Spectrophotometer-integrating-sphere system for computing solar absorptance (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), by William G. Witte, John E. Perry, Wayne S. Slemp, and Langley Research Center (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)
• Experimental evaluation of joint designs for a space-shuttle orbiter ablative leading edge (National Aeronautics and Space Administration ;, 1975), by Stephen S. Tompkins, Walter P. Kabana, and Langley Research Center (page images at HathiTrust)
• Neon transport in selected organic composites (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1984), by Lawrence W. Townsend, Hari B. Bidasaria, John W. Wilson, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Potential use of ceramic coating as a thermal insulation on cooled turbine hardware (National Aeronautics and Space Administration ;, 1976), by Curt H. Liebert, Francis S. Stepka, and Lewis Research Center (page images at HathiTrust)
• Performance of a Haynes 188 metallic standoff thermal protection system at Mach 7 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), by Don E. Avery, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Design and evaluation of active cooling systems for Mach 6 cruise vehicle wings (National Aeronautics and Space Administration ;, 1971), by W. A. McConarty, F. M. Anthony, Langley Research Center, and Bell Aerospace Company (page images at HathiTrust)
• Evaluation of active cooling systems for a Mach 6 hypersonic transport airframe (National Aeronautics and Space Administration ;, 1971), by R. G. Helenbrook, F. M. Anthony, W. A. Mcconarty, Langley Research Center, and Bell Aerospace Company (page images at HathiTrust)
• Development of elastomeric thermal shield materials (National Aeronautics and Space Administration, 1965), by C. M. Dolan, General Electric Company, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Study of heat shielding requirements for manned mars landing and return missions : summary report (National Aeronautics and Space Administration, 1965), by Lockheed Missiles and Space Company (page images at HathiTrust)
• Thin sheet impact (National Aeronautics and Space Administration, 1965), by C. J. Maiden, R. E. Sennett, and A. R. McMillan (page images at HathiTrust)
• Development of an improved coating for polybenzimidazole foam (National Aeronautics and Space Administration ;, 1976), by G. J. Neuner, C. B. Delano, United States National Aeronautics and Space Administration, Acurex Corporation. Aerotherm Division, and Ames Research Center (page images at HathiTrust)
• Reflective superinsulation materials (National Aeronautics and Space Administration ;, 1975), by United States. National Aeronautics and Space Administration. Office of Technology Utilization and Mo.) Midwest Research Institute (Kansas City (page images at HathiTrust)
• Study of critical defects in ablative heat shield systems for the space shuttle (National Aeronautics and Space Administration ;, 1972), by R. L. Thompson, W. E. Driver, Ward D. Rummel, Langley Research Center, and Martin Marietta Denver Aerospace (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)
• Design and fabrication of a radiative actively cooled honeycomb sandwich structural panel for a hypersonic aircraft (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by D. A. Ellis, D. M. Schaeffer, L. L. Pagel, McDonnell Aircraft Company, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Aerobrake concepts for NTP systems study (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by Manuel I. Cruz, Langley Research Center, and TRW Inc. Space and Technology Group (page images at HathiTrust)
• Design, fabrication, and structural testing of a lightweight shadow shield for deep-space application (National Aeronautics and Space Administration ;, 1977), by David Miao, Richard L. DeWitt, James R. Barber, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effect of a surface-to-gap temperature discontinuity on the heat transfer to reusable surface insulation tile gaps (National Aeronautics and Space Administration ;, 1976), by David Throckmorton, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• NASA TN D-5930 (National Aeronautics and Space Administration :, 1970), by Kenneth Sutton, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Apollo ablator thermal performance at superorbital entry velocities (National Aeronautics and Space Administration :, 1970), by Donald M. Curry, Emily W. Stephens, Manned Spacecraft Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-5524 (National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), by Gregory R. Wichorek, Bland A. Stein, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-5696 (National Aeronautics and Space Administration ;, 1970), by George F. Sykes, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-6421 (National Aeronautics and Space Administration:, 1971), by George R. Smolak (page images at HathiTrust)
• NASA TN D-1861 (National Aeronautics and Space Administration :, 1964), by Gregory R. Wichorek, Bland A. Stein, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Apollo experience report : spacecraft heating environment and thermal protection for launch through the atmosphere of the earth (National Aeronautics and Space Administration ;, 1973), by Robert L. Dotts and Manned Spacecraft Center (U.S.) (page images at HathiTrust)
• Analytic and experimental evaluation of shadow shields and their support members for thermal control of space vehicles (National Aeronautics and Space Administration ;, 1974), by Robert J. Boyle, Robert J. Stochl, and Lewis Research Center (page images at HathiTrust)
• NASA TN D-6265 (National Aeronautics and Space Administration ;, 1971), by Elden S. Cornette, Edward M. Sullivan, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Apollo experience report : thermal protection subsystem (National Aeronautics and Space Administration ;, 1974), by James E. Pavlosky, Leslie G. St. Leger, and Lyndon B. Johnson Space Center (page images at HathiTrust)
• NASA TN D-6224 (National Aeronautics and Space Administration ;, 1971), by George E. Sweet, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Experimental and analytical determination of vibration characteristics of corrugated, flexibly supported, heat-shield panels (National Aeronautics and Space Administration ;, 1974), by Huey D. Carden and Langley Research Center (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)
• NASA TN D-6228 (National Aeronautics and Space Administration ;, 1971), by Glenn R. Cowgill, William R. Johnson, Lewis Research Center, and United States National Aeronautics and Space Administration (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)
• Measured catalycities of various candidate space shuttle thermal protection system coatings at low temperatures (National Aeronautics and Space Administration ;, 1973), by Carl D. Scott and Manned Spacecraft Center (U.S.) (page images at HathiTrust)
• An analysis of a charring ablator with thermal nonequilibrium, chemical kinetics, and mass transfer (National Aeronautics and Space Administration ;, 1973), by Ronald K. Clark and Langley Research Center (page images at HathiTrust)
• NASA TN D-6331 (National Aeronautics and Space Administration ;, 1971), by Richard L. DeWitt, Max B. Mellner, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Heat-transfer and pressure measurements of a 1/7-scale model of a Mercury capsule at angles of attack from 0° to ±20° at mach numbers of 3.50 and 4.44 (National Aeronautics and Space Administration, 1961), by Nancy L. Taylor, Paige B. Burbank, Ward F. Hodge, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Experimental study of a hot structure for a reentry vehicle (National Aeronautics and Space Administration, 1961), by Richard A. Pride, Bobbie F. Helms, Dick M. Royster, and Langley Research Center (page images at HathiTrust)
• D140E1 heating rate sensor program closing report (General Electric, Nuclear Materials and Propulsion Operation, 1961), by R. R. Swope, U.S. Atomic Energy Commission, and General Electric Company (page images at HathiTrust)
• Development of an aeroacoustic methodology to evaluate heatshield material performance (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1982., 1982), by A. L. Laganelli, Air Force Flight Dynamics Laboratory (U.S.), Air Force Wright Aeronautical Laboratories, and inc Science Applications (page images at HathiTrust)
• Analytical study of a drag brake control systen for hypersonic vehicles (Wright-Patterson Air Force Base, Ohio : Wright Air Development Division, Air Research and Development Command, United States Air Force, 1960., 1960), by J. E. Hayes, Wallace E. Vander Velde, P. H. Rose, Avco-Everett Research Laboratory, United States. Wright Air Development Division, and United States. Air Force. Air Research and Development Command (page images at HathiTrust)
• Investigation of materials for vacuum insulation up to 4000°F (Wright-Patterson Air Force Base, Ohio : Directorate of Materials and Processes, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1962., 1962), by Peter E. Glaser, Joan Berkowitz, Ivan Simon, Alfred E. Wechsler, United States. Air Force. Systems Command. Aeronautical Systems Division, and Inc Arthur D. Little (page images at HathiTrust)

More items available under broader and related terms at left.