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1Academic Journal
المؤلفون: Martin, Arnold W., Beaulieu, Warren D., Flight Research Center (U.S.), North American Rockwell Corporation.
مصطلحات موضوعية: Simulation methods, Airplanes, Military, B-70 bomber, Tables (data), Pressure drop, Performance prediction, Flight simulation, Atmospheric turbulence, Transient pressures, Inlet flow, Flight tests, B-70 aircraft
وصف الملف: bib
Relation: Also available online from the NASA Technical Reports Server (http://ntrs.nasa.gov/). Address as of 12/15/05: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19700022266%5f1970022266.pdf.; http://hdl.handle.net/2027/uiug.30112106859736
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2Academic Journal
المساهمون: NORTH AMERICAN ROCKWELL CORP LOS ANGELES CA LOS ANGELES DIV
المصدر: DTIC AND NTIS
مصطلحات موضوعية: Aerodynamics, Patrol and Reconnaissance Aircraft, Jet and Gas Turbine Engines, (*RECONNAISSANCE AIRCRAFT, TURBOJET ENGINES), (*TURBOJET ENGINES, AXIAL FLOW COMPRESSORS), (*AXIAL FLOW COMPRESSORS, FLOW SEPARATION), STABILITY, TURBULENCE, TURBULENT BOUNDARY LAYER, REYNOLDS NUMBER, STATISTICAL ANALYSIS, PROBABILITY, ANGLE OF ATTACK, WIND TUNNEL MODELS, MATHEMATICAL MODELS, TACTICAL AIR SUPPORT, ADVANCED WEAPONS
وصف الملف: text/html
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3Electronic Resource
المؤلفون: NORTH AMERICAN ROCKWELL CORP LOS ANGELES CA LOS ANGELES DIV, Beaulieu, Warren D., Boyd, Harry E., Jr., Kostin, Leonard C., Martin, Arnold W.
المصدر: DTIC AND NTIS
مصطلحات الفهرس: Aerodynamics, Patrol and Reconnaissance Aircraft, Jet and Gas Turbine Engines, (*RECONNAISSANCE AIRCRAFT, TURBOJET ENGINES), (*TURBOJET ENGINES, AXIAL FLOW COMPRESSORS), (*AXIAL FLOW COMPRESSORS, FLOW SEPARATION), STABILITY, TURBULENCE, TURBULENT BOUNDARY LAYER, REYNOLDS NUMBER, STATISTICAL ANALYSIS, PROBABILITY, ANGLE OF ATTACK, WIND TUNNEL MODELS, MATHEMATICAL MODELS, TACTICAL AIR SUPPORT, ADVANCED WEAPONS., Text