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1دورية أكاديمية
المؤلفون: Kenworthy, M A, Richards, B E
المساهمون: VON KARMAN INST FOR FLUID DYNAMICS RHODE-SAINT-GENESE (BELGIUM)
المصدر: DTIC AND NTIS
مصطلحات موضوعية: Guided Missile Reentry Vehicles, Fluid Mechanics, HYPERSONIC FLOW, NOSE CONES, REENTRY VEHICLES, ABLATION, AERODYNAMIC CONFIGURATIONS, AEROTHERMODYNAMICS, BLUNT BODIES, CONICAL BODIES, HIGH SPEED PHOTOGRAPHY, INSTABILITY, SCHLIEREN PHOTOGRAPHY, SPIKES, TURBULENT BOUNDARY LAYER, TURBULENT FLOW
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2دورية أكاديمية
المؤلفون: Shope, Frederick L
المساهمون: ARNOLD ENGINEERING DEVELOPMENT CENTER ARNOLD AFB TN
المصدر: DTIC AND NTIS
مصطلحات موضوعية: Theoretical Mathematics, Computer Programming and Software, Fluid Mechanics, AERODYNAMIC CONFIGURATIONS, COMPUTER PROGRAMS, NOSES, AIRCRAFT NOSES, FLOW FIELDS, FORTRAN, GEOMETRIC FORMS, INPUT OUTPUT PROCESSING, MATHEMATICAL MODELS, NOSE CAPS, NOSE CONES, PROGRAMMING MANUALS, ROCKET NOSES, KWIKNOSE COMPUTER PROGRAM, LPN-ARO-V33A-A8A, PE65807F
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3دورية أكاديمية
المؤلفون: Maozhao, Yang
المساهمون: FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OH
المصدر: DTIC AND NTIS
مصطلحات موضوعية: Guided Missile Traj, Accuracy and Ballistics, SHAPE, ABLATION, NOSE CONES, PREDICTIONS, MODIFICATION, DIFFERENCE EQUATIONS, ACCURACY, FINITE DIFFERENCE THEORY, TRANSLATIONS, NUMERICAL METHODS AND PROCEDURES, VISCOSITY, AERODYNAMIC HEATING, CHINA, CHINESE LANGUAGE, ATMOSPHERE ENTRY, FOREIGN TECHNOLOGY, AERODYNAMIC CONFIGURATIONS, CONTROL
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4دورية أكاديمية
المؤلفون: Greenhalgh,Samuel
المساهمون: NAVAL AIR DEVELOPMENT CENTER WARMINSTER PA AIRCRAFT AND CREW SYSTEMS TECHNOLOGY DIRECTORATE
المصدر: DTIC AND NTIS
مصطلحات موضوعية: Fluid Mechanics, AERODYNAMIC FORCES, AERIAL TARGETS, AERODYNAMIC CONFIGURATIONS, AERODYNAMIC STABILITY, ANGLE OF ATTACK, NOSE CONES, AFTERBODIES, TDU-34/A targets, PE64258N, LPN-630-6301/001-d/0W06-100-000
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5دورية أكاديمية
المؤلفون: Ingram,Charles W, Ball,Karlheinz O W, Dinkeloo,Carter, Shida,David
المساهمون: SYSTEMS RESEARCH LABS INC DAYTON OH AEROSYSTEMS RESEARCH DIV
المصدر: DTIC AND NTIS
مصطلحات موضوعية: Guided Missile Dynam, Config & Cntrl Surfaces, Guided Missiles, AERODYNAMIC CONFIGURATIONS, GUIDED MISSILES, AERODYNAMIC CHARACTERISTICS, EXPERIMENTAL DATA, ANGLE OF ATTACK, MATHEMATICAL PREDICTION, COEFFICIENTS, AERODYNAMIC FORCES, WIND TUNNEL TESTS, BLUNT BODIES, TRANSONIC CHARACTERISTICS, NOSE CONES, WUAFFDL24030507, PE62201F
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6دورية أكاديمية
المؤلفون: Kapp, R., Mathauer, H., Rieger, H.
المساهمون: DORNIER G M B H FRIEDRICHSHAFEN (GERMANY F R)
المصدر: DTIC AND NTIS
مصطلحات موضوعية: Fluid Mechanics, Guided Missiles, GUIDED MISSILES, AERODYNAMIC HEATING, HEAT TRANSFER, LAMINAR FLOW, TURBULENT FLOW, GUIDED MISSILE COMPONENTS, FLOW FIELDS, HEAT FLUX, BOUNDARY LAYER, NOSE CONES, BLUNT BODIES, OGIVES, HEMISPHERES, BOUNDARY LAYER TRANSITION, TEMPERATURE, TIME DEPENDENCE, NAVIER STOKES EQUATIONS, SUPERSONIC FLIGHT, SURFACE TEMPERATURE, INTERNAL, AERODYNAMIC CONFIGURATIONS, NUMERICAL ANALYSIS, WEST GERMANY, Parabolized Navier Stoke equations, Semiempirical methods, NATO Furnished, Component Reports
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7دورية أكاديمية
المؤلفون: Ausherman,D. W., Yanta,W. J.
المساهمون: NAVAL SURFACE WEAPONS CENTER SILVER SPRING MD
المصدر: DTIC AND NTIS
مصطلحات موضوعية: GAS FLOW, BOUNDARY LAYER, WIND TUNNEL TESTS, NOSE CONES, BLUNT BODIES, AERODYNAMIC CONFIGURATIONS, THREE DIMENSIONAL, SUPERSONIC WIND TUNNELS, FREE STREAM, DATA BASES, Component reports
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8دورية أكاديمية
المؤلفون: Burleson, W G, Eppes, Jr, R
المساهمون: ARMY MISSILE COMMAND REDSTONE ARSENAL AL SYSTEMS RESEARCH DIRECTORATE
المصدر: DTIC AND NTIS
مصطلحات موضوعية: Theoretical Mathematics, Thermodynamics, CURVED PROFILES, HEAT TRANSFER, AERODYNAMIC CONFIGURATIONS, AERODYNAMIC HEATING, AIRFRAMES, CYLINDRICAL BODIES, EQUATIONS, FLAT PLATE MODELS, GUIDED MISSILES, MATHEMATICAL ANALYSIS, NOSE CONES, NUMERICAL METHODS AND PROCEDURES, ONE DIMENSIONAL FLOW, REENTRY VEHICLES, SELECTION, SPHERES, SURFACE TEMPERATURE, THERMAL PROPERTIES, THERMAL STRESSES, solutions(mathematics)
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9دورية أكاديمية
المؤلفون: Hahn, J S, Little, H R
المساهمون: ARNOLD ENGINEERING DEVELOPMENT CENTER ARNOLD AFB TN
المصدر: DTIC AND NTIS
مصطلحات موضوعية: Guided Missile Dynam, Config & Cntrl Surfaces, Guided Missile Reentry Vehicles, NOSE CONES, ABLATION, AERODYNAMIC CONFIGURATIONS, ANGLE OF ATTACK, BLUNT BODIES, DISTRIBUTION, FORCE(MECHANICS), HYPERSONIC CHARACTERISTICS, MODEL TESTS, MOMENTS, PITCH(MOTION), PRESSURE, REENTRY VEHICLES, REYNOLDS NUMBER, ROLL, SIMULATION, WIND TUNNEL MODELS, YAW
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10دورية أكاديمية
المؤلفون: Olsen, James J
المساهمون: AIR FORCE FLIGHT DYNAMICS LAB WRIGHT-PATTERSON AFB OH
المصدر: DTIC AND NTIS
مصطلحات موضوعية: Fluid Mechanics, Mechanics, FLUTTER, HYPERSONIC FLOW, SUPERSONIC FLOW, AERODYNAMIC CHARACTERISTICS, AERODYNAMIC CONFIGURATIONS, MATHEMATICAL ANALYSIS, NOSE CONES, PANELS, SHOCK WAVES
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