-
1دورية أكاديمية
المؤلفون: Rubin, Donald
المساهمون: ARMY MISSILE RESEARCH DEVELOPMENT AND ENGINEERING LAB REDSTONE ARSENAL AL AEROBALLISTICS DIRECTORATE
المصدر: DTIC AND NTIS
مصطلحات موضوعية: Guided Missile Warheads and Fuzes, GUIDED MISSILE MODELS, AERODYNAMIC DRAG, ANGLE OF ATTACK, BLEED SYSTEMS, BOUNDARY LAYER CONTROL, DRAG REDUCTION, EXPERIMENTAL DATA, FINS, FLOW RATE, GUIDED MISSILE COMPONENTS, INJECTION, MASS FLOW, NITROGEN, NOSE CONES, OGIVES, STABILIZATION SYSTEMS, SUPERSONIC CHARACTERISTICS, SUPERSONIC WIND TUNNELS, TURBULENT BOUNDARY LAYER, WIND TUNNEL TESTS, FLUID INJECTION, PE62303A
وصف الملف: text/html
-
2دورية أكاديمية
المؤلفون: Cahill, David M
المساهمون: ARNOLD ENGINEERING DEVELOPMENT CENTER ARNOLD AFB TN
المصدر: DTIC AND NTIS
مصطلحات موضوعية: Guided Missile Dynam, Config & Cntrl Surfaces, Surface-launched Guided Missiles, INSTRUMENTATION, PRESSURE DISTRIBUTION, SURFACE TO SURFACE MISSILES, Force(Mechanics), Moments, Payload, Payload analyses, Mach number, Angle of attack, Minuteman, Minuteman 3 missiles, Supersonic characteristics, Minuteman instrumented payload delivery system, Nose cones, Transonic characteristics, Wind tunnel models, Model tests, Guided missile models
وصف الملف: text/html
-
3دورية أكاديمية
المؤلفون: Morrison, A. M., Holmes, J. E., Lawrence, W. R.
المساهمون: NAVAL SURFACE WEAPONS CENTER WHITE OAK LAB SILVER SPRING MD
المصدر: DTIC AND NTIS
مصطلحات موضوعية: Guided Missile Dynam, Config & Cntrl Surfaces, PITCH(MOTION), DAMPING, NOSE CONES, COMPUTER PROGRAMS, ANGLE OF ATTACK, SUPERSONIC CHARACTERISTICS, DEGREES OF FREEDOM, EQUATIONS OF MOTION, STABILITY, ONE DEGREE OF FREEDOM
وصف الملف: text/html
-
4دورية أكاديمية
المساهمون: AIR FORCE FLIGHT DYNAMICS LAB WRIGHT-PATTERSON AFB OH
المصدر: DTIC AND NTIS
مصطلحات موضوعية: Aerodynamics, Guided Missiles, GUIDED MISSILES, AERODYNAMIC CHARACTERISTICS, EXPERIMENTAL DATA, SLENDER BODIES, YAW, LOADS(FORCES), WAKE, MACH NUMBER, REYNOLDS NUMBER, NOSE CONES, TRANSONIC CHARACTERISTICS, SUPERSONIC CHARACTERISTICS, SUBSONIC CHARACTERISTICS, WIND TUNNEL TESTS, VORTICES, ANGLE OF ATTACK, VORTEX SHEDDING, FLOW FIELDS, MX MISSILES, PE62201F, WUAFWAL24040701
وصف الملف: text/html
-
5دورية أكاديمية
المؤلفون: Cottrell,Charles J, Chapman,Gary T
المساهمون: AIR FORCE ARMAMENT LAB EGLIN AFB FL
المصدر: DTIC AND NTIS
مصطلحات موضوعية: Fluid Mechanics, TURBULENT BOUNDARY LAYER, FREE STREAM, FLOW SEPARATION, LAMINAR BOUNDARY LAYER, COMPUTATIONS, PARAMETERS, COMPARISON, MOMENTS, VARIATIONS, CYLINDRICAL BODIES, LIMITATIONS, PARABOLAS, MACH NUMBER, FLUID DYNAMICS, SUPERSONIC CHARACTERISTICS, NAVIER STOKES EQUATIONS, PRESSURE DISTRIBUTION, SKIN FRICTION, NOSE CONES, FLARED AFTERBODIES, PE61102F, WUAFATL2307E125
وصف الملف: text/html
-
6دورية أكاديمية
المؤلفون: Devan,Leroy
المساهمون: NAVAL SURFACE WEAPONS CENTER DAHLGREN VA
المصدر: DTIC AND NTIS
مصطلحات موضوعية: Aerodynamics, COMPUTERIZED SIMULATION, AERODYNAMIC CHARACTERISTICS, COMPUTATIONS, PARAMETERS, TAIL ASSEMBLIES, SHOCK WAVES, ANGLE OF ATTACK, COEFFICIENTS, PARTIAL DIFFERENTIAL EQUATIONS, MACH NUMBER, NUMERICAL METHODS AND PROCEDURES, DRAG, SUPERSONIC CHARACTERISTICS, STATICS, INVISCID FLOW, TACTICAL WEAPONS, BODIES, LAGRANGIAN FUNCTIONS, TRANSONIC CHARACTERISTICS, NOSE CONES, BODIES OF REVOLUTION, AS214, PE61153N
وصف الملف: text/html
-
7دورية أكاديمية
المؤلفون: Sturek,Walter B, Mylin,Donald C, Bush,Clarence C
المساهمون: BALLISTIC RESEARCH LABS ABERDEEN PROVING GROUND MD
المصدر: DTIC AND NTIS
مصطلحات موضوعية: Aerodynamics, Fluid Mechanics, SLENDER BODIES, AERODYNAMIC STABILITY, SUPERSONIC CHARACTERISTICS, SPIN STABILIZATION, COMPUTERIZED SIMULATION, TURBULENT FLOW, FINITE DIFFERENCE THEORY, CYLINDRICAL BODIES, AERODYNAMIC DRAG, SPINNING(MOTION), OGIVES, INVISCID FLOW, EXTERIOR BALLISTICS, BOUNDARY LAYER FLOW, THREE DIMENSIONAL FLOW, NOSE CONES, MAGNUS EFFECT
وصف الملف: text/html
-
8دورية أكاديمية
المؤلفون: Wolny,William
المساهمون: LUNDY TECHNICAL CENTER POMPANO BEACH FL
المصدر: DTIC AND NTIS
مصطلحات موضوعية: Pilotless Aircraft, Mfg & Industrial Eng & Control of Product Sys, Countermeasures, Pyrotechnics, CHAFF DISPENSERS, COUNTERMEASURES, DISPENSERS, FLARES, MAINTENANCE, CONTROL SYSTEMS, PAYLOAD, TAIL ASSEMBLIES, CYCLES, INSTALLATION, WEIGHT, EXTERNAL STORES, OPERATION, DRONES, SUPERSONIC CHARACTERISTICS, CHECKOUT PROCEDURES, NOSE CONES, ELECTRIC DETONATORS, SEQUENCE SWITCHES, AN/ALE-44
وصف الملف: text/html
-
9دورية أكاديمية
المساهمون: FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OH
المصدر: DTIC AND NTIS
مصطلحات موضوعية: Fluid Mechanics, Guided Missile Reentry Vehicles, Aircraft, TRANSONIC AIRFOILS, AERODYNAMIC FORCES, NOSE CONES, SHOCK WAVES, CHINA, CHINESE LANGUAGE, TRANSLATIONS, BLUNT BODIES, INTERFERENCE, FINITE ELEMENT ANALYSIS, BLAST WAVES, SUPERSONIC CHARACTERISTICS, FLOW FIELDS
وصف الملف: text/html
-
10دورية أكاديمية
المؤلفون: Cowperthwaite, R. L., McEwan, Michael D.
المساهمون: MCDONNELL AIRCRAFT CO ST LOUIS MO
المصدر: DTIC AND NTIS
مصطلحات موضوعية: Computer Programming and Software, Guided Missiles, Thermodynamics, (*REENTRY VEHICLES, COMPUTER PROGRAMS), ABLATION), SIMULATION, ATMOSPHERE ENTRY, AERODYNAMIC HEATING, CONVECTION(HEAT TRANSFER), CONICAL BODIES, NOSE CONES, COMPUTER PROGRAMMING, SUPERSONIC CHARACTERISTICS, FLOW CHARTING, MATERIALS, MATHEMATICAL PREDICTION, BOUNDARY LAYER TRANSITION, REYNOLDS NUMBER, TEMPERATURE, ENTHALPY, VELOCITY, TWO DIMENSIONAL FLOW, FORTRAN, LOSSES, MASS, envir, info