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 1000
... PRESSURE POINT , AND TANGENTIAL FORCE CHARACTERISTICS OF SLENDER NOSE - CYLINDER CONFIGURATIONS IN THE MACH NUMBER RANGE FROM 0.8 TO 4.0 [ DIE NORMALKRAFT- , DRUCKPUNKT- UND TANGENTIALKRAFTCHARAKTERISTIKEN SCHLANKER BUG - ZYLINDER ...
... PRESSURE POINT , AND TANGENTIAL FORCE CHARACTERISTICS OF SLENDER NOSE - CYLINDER CONFIGURATIONS IN THE MACH NUMBER RANGE FROM 0.8 TO 4.0 [ DIE NORMALKRAFT- , DRUCKPUNKT- UND TANGENTIALKRAFTCHARAKTERISTIKEN SCHLANKER BUG - ZYLINDER ...
Page 1001
... pressure tests on the 20 degree wing . ( Modified author abstract ) GRA N74-17711 # Lockheed - Georgia Co. , Marietta . THEORETICAL AND EXPERIMENTAL INVESTIGATIONS OF VORTEX LIFT CONTROL BY SPANWISE BLOWING . VOLUME 2 : THREE ...
... pressure tests on the 20 degree wing . ( Modified author abstract ) GRA N74-17711 # Lockheed - Georgia Co. , Marietta . THEORETICAL AND EXPERIMENTAL INVESTIGATIONS OF VORTEX LIFT CONTROL BY SPANWISE BLOWING . VOLUME 2 : THREE ...
Page 1002
... pressure gradients are presented . The models had nominal diameters of about 16 in . Gradients of 0 % , 10 % , 20 % , and 40 % of centerline dynamic pressure per foot with centerline velocities of 60 ft / sec and 90 ft / sec were ...
... pressure gradients are presented . The models had nominal diameters of about 16 in . Gradients of 0 % , 10 % , 20 % , and 40 % of centerline dynamic pressure per foot with centerline velocities of 60 ft / sec and 90 ft / sec were ...
Page 1003
... pressure and velocity variation in the separated flow regions surrounding the body , velocity profiles in the displaced flow over the body , and the origin and decay of induced turbulence along the boundaries of the separated regions ...
... pressure and velocity variation in the separated flow regions surrounding the body , velocity profiles in the displaced flow over the body , and the origin and decay of induced turbulence along the boundaries of the separated regions ...
Page 1006
... pressure ratios to provide a technical basis for predicting installed wing thrust loading and for evaluating design wing loading of a particular wing aspect ratios . The flow characteristics of ducting components with relatively high ...
... pressure ratios to provide a technical basis for predicting installed wing thrust loading and for evaluating design wing loading of a particular wing aspect ratios . The flow characteristics of ducting components with relatively high ...
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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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