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1دورية أكاديمية
المؤلفون: Myers, A W, Hahn, J S
المساهمون: ARNOLD ENGINEERING DEVELOPMENT CENTER ARNOLD AFB TN
المصدر: DTIC AND NTIS
مصطلحات موضوعية: Gliders and Parachutes, Atmospheric Physics, Guided Missile Dynam, Config & Cntrl Surfaces, ATMOSPHERE ENTRY, DECELERATION, DROGUE PARACHUTES, AXISYMMETRIC FLOW, CONFIGURATIONS, DEPLOYMENT, DRAG, HIGH ALTITUDE, INSTRUMENTATION, NOSE CONES, OSCILLATION, PERFORMANCE(ENGINEERING), PITOT TUBES, PRESSURE, STABILITY, STRUCTURAL COMPONENTS, TEST METHODS, WAKE, WIND TUNNEL MODELS, STRUTS
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2دورية أكاديمية
المؤلفون: Demetriades, A
المساهمون: PHILCO-FORD CORP NEWPORT BEACH CA SPACE AND RE-ENTRY SYSTEMS DIV
المصدر: DTIC AND NTIS
مصطلحات موضوعية: Guided Missile Dynam, Config & Cntrl Surfaces, WAKE, ANEMOMETERS, ANGLE OF ATTACK, ATMOSPHERE ENTRY, AXISYMMETRIC FLOW, BOUNDARY LAYER TRANSITION, DRAG, ELECTRON DENSITY, EXHAUST NOZZLES, HEAT TRANSFER, MATHEMATICAL ANALYSIS, NOSE CONES, PENETRATION, PLASMA JETS, REENTRY VEHICLES, SHOCK WAVES, SUPERSONIC CHARACTERISTICS, SUPERSONIC FLOW, TEMPERATURE, TEST EQUIPMENT, TEST METHODS, TURBULENCE, TURBULENT BOUNDARY LAYER, TWO DIMENSIONAL FLOW, VELOCITY, VISCOSITY, WIND TUNNEL MODELS, HOT-WIRE ANEMOMETERS
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3دورية أكاديمية
المؤلفون: WARREN, W. R., KAEGI, E. M., HARRIS, C. J., GEIGER, R. E.
المساهمون: GENERAL ELECTRIC CO PHILADELPHIA PA MISSILE AND SPACE DIV
المصدر: DTIC AND NTIS
مصطلحات موضوعية: Test Facilities, Equipment and Methods, Spacecraft Trajectories and Reentry, SHOCK TUNNELS, NOSE CONES, SHOCK TUBES, ATMOSPHERE ENTRY, BOUNDARY LAYER, MODEL TESTS, PRESSURE, HYPERSONIC CHARACTERISTICS, LIFT, HYPERSONIC WIND TUNNELS, WIND TUNNEL MODELS, HYPERSONIC FLOW, RESISTANCE THERMOMETERS, TEST METHODS, SHOCK WAVES, PIEZOELECTRIC GAGES, HEAT TRANSFER, REENTRY VEHICLES
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4دورية أكاديمية
المؤلفون: Ragsdale, William C.
المساهمون: NAVAL ORDNANCE LAB WHITE OAK MD
المصدر: DTIC AND NTIS
مصطلحات موضوعية: Guided Missile Dynam, Config & Cntrl Surfaces, Ammunition and Explosives, HYPERVELOCITY PROJECTILES, TEST METHODS, ANGLE OF ATTACK, FLOW VISUALIZATION, FLOW FIELDS, CYLINDRICAL BODIES, PRESSURE, SUPERSONIC CHARACTERISTICS, FLOW SEPARATION, WIND TUNNEL MODELS, RAMJET INLETS, NOSE CONES, STATIC PRESSURE
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5دورية أكاديمية
المساهمون: KAMAN AIRCRAFT CORP BLOOMFIELD CONN
المصدر: DTIC AND NTIS
مصطلحات موضوعية: ROTORCHUTES, RECOVERABLE BOOSTER ENGINES, ATMOSPHERE ENTRY, RECOVERY, DRAG, FLIGHT PATHS, DESCENT TRAJECTORIES, WEIGHT, STABILITY, DECELERATION, MODEL TESTS, WIND TUNNEL MODELS, TRANSONIC CHARACTERISTICS, TEST METHODS, CENTRIFUGAL FIELDS, PERFORMANCE(ENGINEERING), SPRINGS, LOAD DISTRIBUTION, FLIGHT TESTING, NOSE CONES, MANNED SPACECRAFT, LIFT, TORQUE, MOMENTS, CONTROL, CONTROL SYSTEMS, REENTRY VEHICLES, LANDING, FORCE
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