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1دورية أكاديمية
المؤلفون: Cyran, Fred B
المساهمون: ARNOLD ENGINEERING DEVELOPMENT CENTER ARNOLD AFB TN
المصدر: DTIC AND NTIS
مصطلحات موضوعية: Aerodynamics, Numerical Mathematics, Guided Missile Dynam, Config & Cntrl Surfaces, MATHEMATICAL MODELS, STING MOUNTS, SUBSONIC FLOW, SUPERSONIC FLOW, TRANSONIC FLOW, ANGLE OF ATTACK, BASE PRESSURE, DAMPING, DATA ACQUISITION, DERIVATIVES(MATHEMATICS), DYNAMICS, EXPERIMENTAL DATA, MACH NUMBER, NOSE CONES, PITCH(MOTION), STABILITY, STATIC LOADS, WIND TUNNEL TESTS, YAW, PE65807F
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2دورية 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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3دورية 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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4دورية 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