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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: 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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3مورد إلكتروني
المصدر: DTIC AND NTIS
مصطلحات الفهرس: Fluid Mechanics, AERODYNAMIC FORCES, INTERFERENCE, STING MOUNTS, SUPERSONIC WIND TUNNELS, PITCH(MOTION), LITERATURE SURVEYS, DAMPING, TEST METHODS, TURBULENT BOUNDARY LAYER, WAKE, MACH NUMBER, SUPERSONIC FLOW, BOUNDARY LAYER TRANSITION, OGIVES, OSCILLATION, CONICAL BODIES, REYNOLDS NUMBER, BLUNT BODIES, FORCE(MECHANICS), WIND TUNNEL MODELS, LAMINAR BOUNDARY LAYER, LPN-ARO-V41A-N9A, LPN-ARO-V32A-A1A, LPN-ARO-V41A-J0A, LPN-ARO- V32A-04A, PE65807F, Text