Scientific and Technical Aerospace ReportsNASA, Office of Scientific and Technical Information, 1974 - Aeronautics Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database. |
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Page 1003
... requirements of the detector are developed . Problems with low level wind shear are also examined . Author N74-17727 Deutsche Lufthansa Aktiengesellschaft , Frankfurt am Main ( West Germany ) . Meteorological Dept. AN AIRLINE'S ...
... requirements of the detector are developed . Problems with low level wind shear are also examined . Author N74-17727 Deutsche Lufthansa Aktiengesellschaft , Frankfurt am Main ( West Germany ) . Meteorological Dept. AN AIRLINE'S ...
Page 1004
... requirements and methods for improving the performance of helicopters are examined . Author N74-17737 De Havilland Aircraft Co. , Ltd. , Downsview ( Ontario ) . DATA REQUIREMENTS ON TURBULENCE IN THE EARTH'S ATMOSPHERIC SHEAR LAYER FOR ...
... requirements and methods for improving the performance of helicopters are examined . Author N74-17737 De Havilland Aircraft Co. , Ltd. , Downsview ( Ontario ) . DATA REQUIREMENTS ON TURBULENCE IN THE EARTH'S ATMOSPHERIC SHEAR LAYER FOR ...
Page 1005
... requirements was obtained with a gross weight increase to 226 796 Kg ( 500 000 lb ) . Although wing aeroelastic divergence was a primary design consideration for the yawed - wing concepts , the graphite - epoxy wings of this study were ...
... requirements was obtained with a gross weight increase to 226 796 Kg ( 500 000 lb ) . Although wing aeroelastic divergence was a primary design consideration for the yawed - wing concepts , the graphite - epoxy wings of this study were ...
Page 1007
... requirements for an air cushion landing system in the hover condition . Nine specific nozzle configurations were tested to determine which resulted in the best power - height performance and whether the theory is able to predict the ...
... requirements for an air cushion landing system in the hover condition . Nine specific nozzle configurations were tested to determine which resulted in the best power - height performance and whether the theory is able to predict the ...
Page 1009
... requirements have been raised . However , the method of using aerodynamic corrections to the velocity indicator retained a number of tolerances which were valid earlier . Under modern conditions these tolerances lead to considerable ...
... requirements have been raised . However , the method of using aerodynamic corrections to the velocity indicator retained a number of tolerances which were valid earlier . Under modern conditions these tolerances lead to considerable ...
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aerodynamic Aeronautics and Space Aerospace aircraft analysis analyzed Apollo 17 applications Arlington atmospheric Author GRA Author NSA boundary layer Calif characteristics Corp CSCL 03B Dept described determined developed discussed effects electron emission energy Engineering ENGLISH equations ESRO evaluation experimental Final Report flight flow frequency function heat Includes Inst investigated Johnson Space Center Joint Publications Research Langley Research Center laser materials measurements Meteoroids method Microfilms Order Modified author abstract Moscow NASA National Aeronautics NTIS CSCL NTIS HC obtained Ohio operation optical parameters particles Patent plasma prefs pressure problems Proj Publications Research Service radiation refs Contract refs For availability refs Transl related information Research Center simulation SKYLAB solar Space Administration structure surface techniques Technology temperature thermal turbulence Univ V/STOL velocity Vestn Washington NASA wind tunnel Wright-Patterson AFB
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Page 994 - December, 1964) published by the Committee on Scientific and Technical Information of the Federal Council for Science and Technology.
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