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1دورية أكاديمية
المؤلفون: Greenhalgh,Samuel
المساهمون: NAVAL AIR DEVELOPMENT CENTER WARMINSTER PA AIRCRAFT AND CREW SYSTEMS TECHNOLOGY DIRECTORATE
المصدر: DTIC AND NTIS
مصطلحات موضوعية: Fluid Mechanics, AERODYNAMIC FORCES, AERIAL TARGETS, AERODYNAMIC CONFIGURATIONS, AERODYNAMIC STABILITY, ANGLE OF ATTACK, NOSE CONES, AFTERBODIES, TDU-34/A targets, PE64258N, LPN-630-6301/001-d/0W06-100-000
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2دورية أكاديمية
المؤلفون: Ingram,Charles W, Ball,Karlheinz O W, Dinkeloo,Carter, Shida,David
المساهمون: SYSTEMS RESEARCH LABS INC DAYTON OH AEROSYSTEMS RESEARCH DIV
المصدر: DTIC AND NTIS
مصطلحات موضوعية: Guided Missile Dynam, Config & Cntrl Surfaces, Guided Missiles, AERODYNAMIC CONFIGURATIONS, GUIDED MISSILES, AERODYNAMIC CHARACTERISTICS, EXPERIMENTAL DATA, ANGLE OF ATTACK, MATHEMATICAL PREDICTION, COEFFICIENTS, AERODYNAMIC FORCES, WIND TUNNEL TESTS, BLUNT BODIES, TRANSONIC CHARACTERISTICS, NOSE CONES, WUAFFDL24030507, PE62201F
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3دورية أكاديمية
المؤلفون: Hahn, J S, Little, H R
المساهمون: ARNOLD ENGINEERING DEVELOPMENT CENTER ARNOLD AFB TN
المصدر: DTIC AND NTIS
مصطلحات موضوعية: Guided Missile Dynam, Config & Cntrl Surfaces, Guided Missile Reentry Vehicles, NOSE CONES, ABLATION, AERODYNAMIC CONFIGURATIONS, ANGLE OF ATTACK, BLUNT BODIES, DISTRIBUTION, FORCE(MECHANICS), HYPERSONIC CHARACTERISTICS, MODEL TESTS, MOMENTS, PITCH(MOTION), PRESSURE, REENTRY VEHICLES, REYNOLDS NUMBER, ROLL, SIMULATION, WIND TUNNEL MODELS, YAW
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4دورية أكاديمية
المؤلفون: Hughes, Joseph M
المساهمون: ARMY BALLISTIC RESEARCH LAB ABERDEEN PROVING GROUND MD
المصدر: DTIC AND NTIS
مصطلحات موضوعية: Guided Missile Dynam, Config & Cntrl Surfaces, Guided Missiles, GUIDED MISSILE TARGETS, AERODYNAMIC CONFIGURATIONS, ANGLE OF ATTACK, CONICAL BODIES, DEFLECTION, DRAG, FINS, MODEL TESTS, MOMENTS, NOSE CONES, PITCH(MOTION), ROCKET MODELS, ROLL, SCALE, SCHLIEREN PHOTOGRAPHY, SHOCK WAVES, SUPERSONIC CHARACTERISTICS, WIND TUNNEL MODELS, CENTER OF PRESSURE, DEFENDER PROJECT, GRAPHS(CHARTS)
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5دورية أكاديمية
المؤلفون: Brick, L.
المساهمون: LOCKHEED MISSILES AND SPACE CO INC SUNNYVALE CA
المصدر: DTIC AND NTIS
مصطلحات موضوعية: Computer Programming and Software, Guided Missile Reentry Vehicles, NOSE CONES, COMPUTER PROGRAMS, DATA PROCESSING, MATERIALS, STRUCTURAL PROPERTIES, ABLATION, REENTRY VEHICLES, ATMOSPHERE ENTRY, MATHEMATICAL PREDICTION, AERODYNAMIC CONFIGURATIONS, ANGLE OF ATTACK, SURFACE ROUGHNESS, HEAT TRANSFER, AERODYNAMIC HEATING, BOUNDARY LAYER TRANSITION, AERODYNAMIC LOADING, CONTINUUM MECHANICS, GRAPHITE, THICKNESS, SURFACE TEMPERATURE, REINFORCING MATERIALS, MATHEMATICAL MODELS, DIFFERENTIAL EQUATIONS, PHENOLIC PLASTICS, SILICON DIOXIDE, CARBON COMPOUNDS, THERMAL STRESSES, ABLATIVE MATERIALS
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6دورية أكاديمية
المؤلفون: Williams, Edgar P., Inger, George R.
المساهمون: MCDONNELL DOUGLAS ASTRONAUTICS CO-HB HUNTINGTON BEACH CA
المصدر: DTIC AND NTIS
مصطلحات موضوعية: Guided Missile Dynam, Config & Cntrl Surfaces, (*ABLATION, SURFACE PROPERTIES), AERODYNAMIC CONFIGURATIONS, WALLS, NOSE CONES, CONICAL BODIES, SURFACE TEMPERATURE, HEAT TRANSFER, TURBULENT BOUNDARY LAYER, AERODYNAMIC LOADING, PRESSURE, ROLL, CRYSTALS, LIQUIDS, REFRACTORY COATINGS, COOLING, PRANDTL NUMBER, TRANSONIC FLOW, HYPERSONIC FLOW, WIND TUNNEL MODELS, INSTRUMENTATION, ANGLE OF ATTACK, MOMENTS, AERODYNAMIC CHARACTERISTICS, AERODYNAMIC HEATING, MODEL TESTS, ABLATION SURFACE CROSS HATCHING PROGRAM, CAMPHOR
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7دورية أكاديمية
المؤلفون: Katskova,O. N., Chushkin,P. I.
المساهمون: JOHNS HOPKINS UNIV SILVER SPRING MD APPLIED PHYSICS LAB
المصدر: DTIC AND NTIS
مصطلحات موضوعية: Guided Missiles, Fluid Mechanics, (*REENTRY VEHICLES, SUPERSONIC CHARACTERISTICS), THREE DIMENSIONAL FLOW, NUMERICAL METHODS AND PROCEDURES, MATHEMATICAL PREDICTION, ANGLE OF ATTACK, SHOCK WAVES, DUCTED BODIES, AERODYNAMIC CONFIGURATIONS, NOSE CONES, FLOW FIELDS, EQUATIONS OF MOTION, VELOCITY, APPROXIMATION(MATHEMATICS), DIFFERENTIAL EQUATIONS, LEADING EDGES, PRESSURE, METHOD OF CHARACTERISTICS
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8دورية أكاديمية
المؤلفون: Regan, Frank J.
المساهمون: NAVAL ORDNANCE LAB WHITE OAK MD
المصدر: DTIC AND NTIS
مصطلحات موضوعية: Guided Missile Dynam, Config & Cntrl Surfaces, Aerial Bombs, (*BOMB FINS, AERODYNAMIC CHARACTERISTICS), (*BOMBS, STABILITY), (*STABILIZATION SYSTEMS, BOMBS), STABILITY, NOSE CONES, OGIVES, AERODYNAMIC CONFIGURATIONS, DRAG, FORCE(MECHANICS), MOMENTS, AERODYNAMIC LOADING, PITCH(MOTION), DAMPING, ANGLE OF ATTACK, ROLL, YAW, WIND TUNNEL MODELS, MODEL TESTS, PERFORMANCE(ENGINEERING), EXPERIMENTAL DATA, SUBSONIC CHARACTERISTICS, TRANSONIC CHARACTERISTICS, SUPERSONIC CHARACTERISTICS
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