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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 أكاديمية
المؤلفون: Cyran, Fred B, Uselton, Bob L, Marquart, Ed J
المساهمون: ARNOLD ENGINEERING DEVELOPMENT CENTER ARNOLD AFB TN
المصدر: DTIC AND NTIS
مصطلحات موضوعية: Couplers, Fasteners, and Joints, Fluid Mechanics, CONICAL BODIES, STING MOUNTS, SUBSONIC FLOW, TRANSONIC FLOW, ANGLE OF ATTACK, BASE PRESSURE, BLUNT BODIES, BOUNDARY LAYER TRANSITION, DAMPING, LENGTH, PITCH(MOTION), REYNOLDS NUMBER, STABILITY, STATICS, SUBSONIC WIND TUNNELS, SUPPORTS, TEST METHODS, TRANSONIC WIND TUNNELS, TURBULENT BOUNDARY LAYER, PE65807F
وصف الملف: text/html
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3دورية أكاديمية
المؤلفون: Uselton, Bob L, Cyran, Fred B
المساهمون: ARNOLD ENGINEERING DEVELOPMENT CENTER ARNOLD AFB TN
المصدر: DTIC AND NTIS
مصطلحات موضوعية: Fluid Mechanics, AERODYNAMIC FORCES, INTERFERENCE, STING MOUNTS, SUPERSONIC WIND TUNNELS, BLUNT BODIES, BOUNDARY LAYER TRANSITION, CONICAL BODIES, DAMPING, FORCE(MECHANICS), LAMINAR BOUNDARY LAYER, LITERATURE SURVEYS, MACH NUMBER, OGIVES, OSCILLATION, PITCH(MOTION), REYNOLDS NUMBER, SUPERSONIC FLOW, TEST METHODS, TURBULENT BOUNDARY LAYER, WAKE, WIND TUNNEL MODELS, LPN-ARO-V41A-N9A, LPN-ARO-V32A-A1A, LPN-ARO-V41A-J0A, LPN-ARO-V32A-04A, PE65807F
وصف الملف: text/html
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4دورية أكاديمية
المؤلفون: Uselton, Bob L
المساهمون: ARO INC ARNOLD AFS TN
المصدر: DTIC AND NTIS
مصطلحات موضوعية: Guided Missile Dynam, Config & Cntrl Surfaces, Air- and Space-launched Guided Missiles, AIR TO SURFACE MISSILES, SUPERSONIC FLOW, WIND TUNNEL TESTS, ANGLE OF ATTACK, MOTION, REYNOLDS NUMBER, WIND TUNNEL MODELS, IMPULSE CORRECTION GUIDANCE SYSTEM
وصف الملف: text/html
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5دورية أكاديمية
المؤلفون: Uselton, Bob L, Uselton, James C
المساهمون: ARNOLD ENGINEERING DEVELOPMENT CENTER ARNOLD AFB TN
المصدر: DTIC AND NTIS
مصطلحات موضوعية: Guided Missiles, GUIDED MISSILES, PITCH(MOTION), AERODYNAMIC STABILITY, ANGLE OF ATTACK, ASPECT RATIO, DAMPING, SUPERSONIC FLOW, WIND TUNNEL MODELS
وصف الملف: text/html
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6دورية أكاديمية
المؤلفون: Uselton, Bob L, Jenke, Leroy M
المساهمون: ARNOLD ENGINEERING DEVELOPMENT CENTER ARNOLD AFB TN
المصدر: DTIC AND NTIS
مصطلحات موضوعية: Astronautics, Manned Spacecraft, SPACE SHUTTLES, SUPERSONIC CHARACTERISTICS, ANGLE OF ATTACK, DAMPING, PITCH(MOTION), WIND TUNNEL MODELS, YAW, 089 ORBITERS, 089B ORBITERS
وصف الملف: text/html
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7دورية أكاديمية
المؤلفون: Uselton,James C., Uselton,Bob L., Helmlinger,K. R.
المساهمون: ARNOLD ENGINEERING DEVELOPMENT CENTER ARNOLD AIR FORCE STATION TENN
المصدر: DTIC AND NTIS
مصطلحات موضوعية: Test Facilities, Equipment and Methods, MEASUREMENT, STABILITY, WIND TUNNEL MODELS, DAMPING, ANGLE OF ATTACK, COMPUTER APPLICATIONS, OSCILLATION, SUPERSONIC WIND TUNNELS
وصف الملف: text/html
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8دورية أكاديمية
المؤلفون: Uselton, Bob L, Wallace, Arthur R
المساهمون: ARNOLD ENGINEERING DEVELOPMENT CENTER ARNOLD AFB TN
المصدر: DTIC AND NTIS
مصطلحات موضوعية: Unmanned Spacecraft, Spacecraft Trajectories and Reentry, MARS(PLANET), SPACE PROBES, ANGLE OF ATTACK, DECELERATION, RETRO ROCKETS, SOFT LANDINGS, STABILITY, SUPERSONIC FLOW, WIND TUNNEL MODELS, VIKING, DECELERATORS
وصف الملف: text/html