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1دورية أكاديمية
المؤلفون: Pick,George S.
المساهمون: NAVAL SHIP RESEARCH AND DEVELOPMENT CENTER BETHESDA MD AVIATION AND SURFACE EFFECTS DEPT
المصدر: DTIC AND NTIS
مصطلحات موضوعية: Guided Missile Dynam, Config & Cntrl Surfaces, CYLINDRICAL BODIES, LIFT, TEST METHODS, TURBULENT BOUNDARY LAYER, ANGLE OF ATTACK, FLOW VISUALIZATION, MODEL TESTS, WIND TUNNEL TESTS, DATA ACQUISITION, BLUNT BODIES, LAMINAR BOUNDARY LAYER, TRANSONIC CHARACTERISTICS, NOSE CONES, Fineness ratio
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2دورية أكاديمية
المؤلفون: Wray, K L, Rose, P H, Koritz, H E
المساهمون: AVCO EVERETT RESEARCH LAB INC EVERETT MA
المصدر: DTIC AND NTIS
مصطلحات موضوعية: Guided Missile Reentry Vehicles, Unmanned Spacecraft, REENTRY VEHICLES, ABLATION, BOUNDARY LAYER, CONTAMINATION, HALOCARBON PLASTICS, HIGH TEMPERATURE, INFRARED SPECTRA, INTENSITY, MODEL TESTS, NITROGEN, NOSE CONES, PHOTOMULTIPLIER TUBES, SIMULATION, SPECTROPHOTOMETERS, SPECTROSCOPY, SPECTRUM ANALYZERS, TEST METHODS, THERMAL RADIATION, TURBULENT BOUNDARY LAYER, TWO DIMENSIONAL FLOW, ULTRAVIOLET SPECTRA, VISIBLE SPECTRA, DELRIN, TETRAFLUOROETHYLENE RESINS
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3دورية أكاديمية
المؤلفون: Demetriades, A
المساهمون: PHILCO-FORD CORP NEWPORT BEACH CA SPACE AND RE-ENTRY SYSTEMS DIV
المصدر: DTIC AND NTIS
مصطلحات موضوعية: Guided Missile Dynam, Config & Cntrl Surfaces, WAKE, ANEMOMETERS, ANGLE OF ATTACK, ATMOSPHERE ENTRY, AXISYMMETRIC FLOW, BOUNDARY LAYER TRANSITION, DRAG, ELECTRON DENSITY, EXHAUST NOZZLES, HEAT TRANSFER, MATHEMATICAL ANALYSIS, NOSE CONES, PENETRATION, PLASMA JETS, REENTRY VEHICLES, SHOCK WAVES, SUPERSONIC CHARACTERISTICS, SUPERSONIC FLOW, TEMPERATURE, TEST EQUIPMENT, TEST METHODS, TURBULENCE, TURBULENT BOUNDARY LAYER, TWO DIMENSIONAL FLOW, VELOCITY, VISCOSITY, WIND TUNNEL MODELS, HOT-WIRE ANEMOMETERS
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4دورية أكاديمية
المؤلفون: ROLLIN,VERN G.
المساهمون: NATIONAL AERONAUTICS AND SPACE ADMINISTRATION WASHINGTON D C
المصدر: DTIC AND NTIS
مصطلحات موضوعية: GLASS TEXTILES, NOSE CONES, ROCKET ENGINE NOISE, ROCKET NOSES, SOUND TRANSMISSION, ACOUSTICS, CONICAL BODIES, ELECTRONIC EQUIPMENT, HEMISPHERICAL SHELLS, NOISE, TEST EQUIPMENT, TEST METHODS, TURBULENT BOUNDARY LAYER
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5دورية أكاديمية
المؤلفون: Richards,Bryan E.
المساهمون: VON KARMAN INST FOR FLUID DYNAMICS RHODE-SAINT-GENESE (BELGIUM)
المصدر: DTIC AND NTIS
مصطلحات موضوعية: Guided Missile Reentry Vehicles, Thermodynamics, Reentry vehicles, Hypersonic characteristics, Nose cones, Heat transfer, Reynolds number, Aerodynamic configurations, Hemispheres, Conical bodies, Surface roughness, Boundary layer transition, Test methods, Test equipment, Pressure measurement, Laminar boundary layer, Turbulent boundary layer
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