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1دورية أكاديمية
المؤلفون: Burleson, W G, Eppes, Jr, R
المساهمون: ARMY MISSILE COMMAND REDSTONE ARSENAL AL SYSTEMS RESEARCH DIRECTORATE
المصدر: DTIC AND NTIS
مصطلحات موضوعية: Theoretical Mathematics, Thermodynamics, CURVED PROFILES, HEAT TRANSFER, AERODYNAMIC CONFIGURATIONS, AERODYNAMIC HEATING, AIRFRAMES, CYLINDRICAL BODIES, EQUATIONS, FLAT PLATE MODELS, GUIDED MISSILES, MATHEMATICAL ANALYSIS, NOSE CONES, NUMERICAL METHODS AND PROCEDURES, ONE DIMENSIONAL FLOW, REENTRY VEHICLES, SELECTION, SPHERES, SURFACE TEMPERATURE, THERMAL PROPERTIES, THERMAL STRESSES, solutions(mathematics)
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2دورية أكاديمية
المؤلفون: JOHNSON, C H, SMITH, WILLIAM H, KATZ, J R
المساهمون: NAVAL ORDNANCE TEST STATION CHINA LAKE CA
المصدر: DTIC AND NTIS
مصطلحات موضوعية: Fluid Mechanics, AERODYNAMIC HEATING, ANALOG COMPUTERS, GUIDED MISSILES, HEAT TRANSFER, FUNCTIONS(MATHEMATICS), HEATING, MATHEMATICAL ANALYSIS, MODEL TESTS, NOSE CONES, PARTIAL DIFFERENTIAL EQUATIONS, PROPELLANT GRAINS, ROCKET ENGINES, ROCKET PROPELLANTS, SIMULATION, SURFACE TEMPERATURE, TEMPERATURE, TEST METHODS, THERMAL INSULATION, THICKNESS, sidewinder, hpag rocket motor
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3دورية أكاديمية
المؤلفون: Burleson, W G, Reynolds, R A
المساهمون: ARMY MISSILE COMMAND REDSTONE ARSENAL AL SYSTEMS RESEARCH DIRECTORATE
المصدر: DTIC AND NTIS
مصطلحات موضوعية: Fluid Mechanics, AERODYNAMIC HEATING, REENTRY VEHICLES, ABLATION, AIRFRAMES, ALUMINUM, ANTIMISSILE DEFENSE SYSTEMS, ATMOSPHERE ENTRY, BASE FLOW, BLUNT BODIES, CONICAL BODIES, DRAG, EQUATIONS, GLASS, GRAPHICS, GUIDED MISSILE TRAJECTORIES, HEAT SHIELDS, HEAT TRANSFER, MATHEMATICAL ANALYSIS, NOSE CONES, PHENOLIC PLASTICS, RADAR, RECOVERY, SEPARATION, SURFACE TEMPERATURE, TABLES(DATA), THEORY, THERMAL INSULATION, THICKNESS, VOLUME
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4دورية أكاديمية
المؤلفون: BLAND,WILLIAM M. JR., COLLIE,KATHERINE A.
المساهمون: NATIONAL AERONAUTICS AND SPACE ADMINISTRATION WASHINGTON D C
المصدر: DTIC AND NTIS
مصطلحات موضوعية: AERODYNAMIC CONFIGURATIONS, AERODYNAMIC HEATING, ATMOSPHERE ENTRY, HEAT TRANSFER, HYPERSONIC CHARACTERISTICS, NOSE CONES, ROCKET MODELS, AERODYNAMIC CHARACTERISTICS, BODIES OF REVOLUTION, CYLINDRICAL BODIES, FLIGHT TESTING, HYPERSONIC VEHICLES, MATHEMATICAL ANALYSIS, MODEL TESTS, REENTRY VEHICLES, SURFACE TEMPERATURE
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5دورية أكاديمية
المؤلفون: Dore, F. J.
المساهمون: GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA
المصدر: DTIC AND NTIS
مصطلحات موضوعية: Surface-launched Guided Missiles, Thermodynamics, ATMOSPHERE ENTRY), THERMAL STRESSES), (*SURFACE TO SURFACE MISSILES, (*NOSE CONES, REENTRY VEHICLES, TELEMETERING DATA, ACCURACY, AERODYNAMIC HEATING, HEAT TRANSFER, LAMINAR BOUNDARY LAYER, ANGLE OF ATTACK, DRAG, SURFACE TEMPERATURE, MATHEMATICAL ANALYSIS, CONICAL BODIES, PRESSURE, TITAN
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