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1دورية أكاديمية
المؤلفون: Uselton, Bob L, Cyran, Fred B
المساهمون: ARNOLD ENGINEERING DEVELOPMENT CENTER ARNOLD AFB TN
المصدر: DTIC AND NTIS
مصطلحات موضوعية: Test Facilities, Equipment and Methods, Guided Missile Dynam, Config & Cntrl Surfaces, BLUNT BODIES, HYPERSONIC VELOCITY, SUPERSONIC FLOW, WIND TUNNEL TESTS, ANGLE OF ATTACK, BASE PRESSURE, DAMPING, DYNAMIC TESTS, INTERFERENCE, LAMINAR BOUNDARY LAYER, MACH NUMBER, MEASUREMENT, NOSE CONES, OSCILLATION, PITCH(MOTION), STATIC STABILITY, STING MOUNTS, TURBULENT BOUNDARY LAYER, WIND TUNNEL MODELS, LPN-ARO-V41A/B-W4A, LPN-ARO-V32F-09, LPN-ARO-V32A-A1A, LPN-ARO-41A/B-N9A, LPN-ARO-V32A-R0A, PE65807F
وصف الملف: text/html
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2دورية أكاديميةStatic Stability and Axial Force Tests of the Holloman Monorail Rocket Sled at Mach Numbers 8 and 10
المؤلفون: Rhudy, R W, Corce, J D
المساهمون: ARNOLD ENGINEERING DEVELOPMENT CENTER ARNOLD AFB TN
المصدر: DTIC AND NTIS
مصطلحات موضوعية: Test Facilities, Equipment and Methods, AERODYNAMIC CHARACTERISTICS, ROCKET SLEDS, AERODYNAMIC FORCES, BOUNDARY LAYER, CANARD CONFIGURATIONS, FLOW VISUALIZATION, HYPERSONIC CHARACTERISTICS, HYPERSONIC WIND TUNNELS, INTERACTIONS, NOSE CONES, SHOCK WAVES, STATIC STABILITY, WIND TUNNEL MODELS, WIND TUNNEL TESTS, Monorail rocket sleds
وصف الملف: text/html
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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
وصف الملف: text/html
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4دورية أكاديمية
المؤلفون: FITZGERALD, JR., PAUL E.
المساهمون: NATIONAL AERONAUTICS AND SPACE ADMIN LANGLEY RESEARCH CENTER HAMPTON VA
المصدر: DTIC
مصطلحات موضوعية: Test Facilities, Equipment and Methods, Guided Missile Dynam, Config & Cntrl Surfaces, Guided Missiles, REENTRY VEHICLES, PITCH(MOTION), SHOCK WAVES, HYPERSONIC CHARACTERISTICS, MOMENTS, PRESSURE, CONICAL BODIES, WIND TUNNEL MODELS, SCHLIEREN PHOTOGRAPHY, NOSE CONES, PITCH(MATERIAL)
وصف الملف: text/html