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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
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2دورية أكاديمية
المؤلفون: Ward,L C
المساهمون: ROYAL AIRCRAFT ESTABLISHMENT FARNBOROUGH (ENGLAND)
المصدر: DTIC AND NTIS
مصطلحات موضوعية: Test Facilities, Equipment and Methods, Guided Missile Dynam, Config & Cntrl Surfaces, CONICAL BODIES, SUPERSONIC FLOW, BLUNT BODIES, PRESSURE DISTRIBUTION, SHARP BODIES, WIND TUNNEL TESTS, ANGLE OF ATTACK, BODIES OF REVOLUTION, FRONT ENDS AND SURFACES, AXISYMMETRIC, NOSE CONES, PRESSURE MEASUREMENT, EXPERIMENTAL DATA, TABLES(DATA), UNITED KINGDOM, Forebodies, Surface pressure
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3دورية أكاديمية
المؤلفون: Stetson, Kenneth F.
المساهمون: AVCO GOVERNMENT PRODUCTS GROUP WILMINGTON MA AVCO MISSILE SYSTEMS DIV
المصدر: DTIC AND NTIS
مصطلحات موضوعية: Test Facilities, Equipment and Methods, Fluid Mechanics, SHOCK TUBES, LAMINAR BOUNDARY LAYER, GEOMETRIC FORMS, PRESSURE, MACH NUMBER, SUPERSONIC FLOW, CONICAL BODIES, REYNOLDS NUMBER, BLUNT BODIES, HYPERSONIC FLOW, THREE DIMENSIONAL FLOW, NOSE CONES, PIEZOELECTRIC TRANSDUCERS, HEAT TRANSFER, ANGLE OF ATTACK, SHARP BODIES
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