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1دورية أكاديمية
المؤلفون: Pick,George S.
المساهمون: NAVAL SHIP RESEARCH AND DEVELOPMENT CENTER BETHESDA MD AVIATION AND SURFACE EFFECTS DEPT
المصدر: DTIC AND NTIS
مصطلحات موضوعية: Guided Missile Dynam, Config & Cntrl Surfaces, CYLINDRICAL BODIES, LIFT, TEST METHODS, TURBULENT BOUNDARY LAYER, ANGLE OF ATTACK, FLOW VISUALIZATION, MODEL TESTS, WIND TUNNEL TESTS, DATA ACQUISITION, BLUNT BODIES, LAMINAR BOUNDARY LAYER, TRANSONIC CHARACTERISTICS, NOSE CONES, Fineness ratio
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2دورية أكاديمية
المؤلفون: Johnson,Elmer G, Von Ohain,Hans J P
المساهمون: DEPARTMENT OF THE AIR FORCE WASHINGTON D C
المصدر: DTIC AND NTIS
مصطلحات موضوعية: Test Facilities, Equipment and Methods, Guided Missile Dynam, Config & Cntrl Surfaces, Atmosphere entry, Test methods, Patents, Particle accelerator techniques, Enthalpy, Nozzles, Nose cones, Arc heaters, PAT-CL-73-147
وصف الملف: text/html
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3دورية 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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4دورية 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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5دورية 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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