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1دورية 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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2دورية 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)
وصف الملف: text/html
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3دورية أكاديمية
المؤلفون: BLAND,WILLIAM M. JR., COLLIE,KATHERINE A.
المساهمون: NATIONAL AERONAUTICS AND SPACE ADMINISTRATION WASHINGTON D C
المصدر: DTIC AND NTIS
مصطلحات موضوعية: AERODYNAMIC CONFIGURATIONS, AERODYNAMIC HEATING, ATMOSPHERE ENTRY, HEAT TRANSFER, HYPERSONIC CHARACTERISTICS, NOSE CONES, ROCKET MODELS, AERODYNAMIC CHARACTERISTICS, BODIES OF REVOLUTION, CYLINDRICAL BODIES, FLIGHT TESTING, HYPERSONIC VEHICLES, MATHEMATICAL ANALYSIS, MODEL TESTS, REENTRY VEHICLES, SURFACE TEMPERATURE
وصف الملف: text/html
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4دورية أكاديمية
المؤلفون: Brick, L.
المساهمون: LOCKHEED MISSILES AND SPACE CO INC SUNNYVALE CA
المصدر: DTIC AND NTIS
مصطلحات موضوعية: Computer Programming and Software, Guided Missile Reentry Vehicles, NOSE CONES, COMPUTER PROGRAMS, DATA PROCESSING, MATERIALS, STRUCTURAL PROPERTIES, ABLATION, REENTRY VEHICLES, ATMOSPHERE ENTRY, MATHEMATICAL PREDICTION, AERODYNAMIC CONFIGURATIONS, ANGLE OF ATTACK, SURFACE ROUGHNESS, HEAT TRANSFER, AERODYNAMIC HEATING, BOUNDARY LAYER TRANSITION, AERODYNAMIC LOADING, CONTINUUM MECHANICS, GRAPHITE, THICKNESS, SURFACE TEMPERATURE, REINFORCING MATERIALS, MATHEMATICAL MODELS, DIFFERENTIAL EQUATIONS, PHENOLIC PLASTICS, SILICON DIOXIDE, CARBON COMPOUNDS, THERMAL STRESSES, ABLATIVE MATERIALS
وصف الملف: text/html
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5دورية أكاديمية
المؤلفون: Brick, L.
المساهمون: LOCKHEED MISSILES AND SPACE CO INC SUNNYVALE CA
المصدر: DTIC AND NTIS
مصطلحات موضوعية: Computer Programming and Software, Guided Missile Reentry Vehicles, NOSE CONES, COMPUTER PROGRAMS, STRUCTURAL PROPERTIES, MATERIALS, ABLATION, REENTRY VEHICLES, ATMOSPHERE ENTRY, MATHEMATICAL PREDICTION, MATHEMATICAL MODELS, DIFFERENTIAL EQUATIONS, CONTINUUM MECHANICS, THERMAL STRESSES, ENTHALPY, STAGNATION POINT, COMPOSITE MATERIALS, THICKNESS, GRAPHITE, CARBON FIBERS, PHASE STUDIES, QUARTZ, CARBON, PHENOLIC PLASTICS, SENSITIVITY, SURFACE TEMPERATURE, BOUNDARY LAYER TRANSITION, AERODYNAMIC CONFIGURATIONS, DATA PROCESSING, 3DQP
وصف الملف: text/html
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6دورية أكاديمية
المؤلفون: Williams, Edgar P., Inger, George R.
المساهمون: MCDONNELL DOUGLAS ASTRONAUTICS CO-HB HUNTINGTON BEACH CA
المصدر: DTIC AND NTIS
مصطلحات موضوعية: Guided Missile Dynam, Config & Cntrl Surfaces, (*ABLATION, SURFACE PROPERTIES), AERODYNAMIC CONFIGURATIONS, WALLS, NOSE CONES, CONICAL BODIES, SURFACE TEMPERATURE, HEAT TRANSFER, TURBULENT BOUNDARY LAYER, AERODYNAMIC LOADING, PRESSURE, ROLL, CRYSTALS, LIQUIDS, REFRACTORY COATINGS, COOLING, PRANDTL NUMBER, TRANSONIC FLOW, HYPERSONIC FLOW, WIND TUNNEL MODELS, INSTRUMENTATION, ANGLE OF ATTACK, MOMENTS, AERODYNAMIC CHARACTERISTICS, AERODYNAMIC HEATING, MODEL TESTS, ABLATION SURFACE CROSS HATCHING PROGRAM, CAMPHOR
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