Scientific and Technical Aerospace Reports, 29. sējums,1-3. izdevumsScientific and Technical Information Office, National Aeronautics and Space Administration, 1991 |
No grāmatas satura
1.–5. rezultāts no 100.
1. lappuse
... pressure in the piping , influence by the twisting and warping of the piping as a result of a change in the stance of the model , influence by the division of air power between the balance and the piping due rigidity of the piping ...
... pressure in the piping , influence by the twisting and warping of the piping as a result of a change in the stance of the model , influence by the division of air power between the balance and the piping due rigidity of the piping ...
5. lappuse
... pressure and total pressure is discussed in connection with the streamlines for the primary vortex . ESA N91-10027 # Deutsche Forschungsanstalt fuer Luft- und Raumfahrt , Cologne ( Germany , F.R. ) . Hauptabt . Windkanaele . WIND TUNNEL ...
... pressure and total pressure is discussed in connection with the streamlines for the primary vortex . ESA N91-10027 # Deutsche Forschungsanstalt fuer Luft- und Raumfahrt , Cologne ( Germany , F.R. ) . Hauptabt . Windkanaele . WIND TUNNEL ...
10. lappuse
... pressure and flow angles . It may be concluded that there are some reductions in total pressure losses and increases in outlet flow angles in the tip region caused by the coolant injection . NASDA N91-10061 * # Ohio State Univ ...
... pressure and flow angles . It may be concluded that there are some reductions in total pressure losses and increases in outlet flow angles in the tip region caused by the coolant injection . NASDA N91-10061 * # Ohio State Univ ...
11. lappuse
... pressure , radiation - heated gas over an annular shroud surface . The blast waves are generated by laser radiation heating of air using Laser Supported Detonation ( LSD ) waves . The phenomenology of LSD waves is described , as is the ...
... pressure , radiation - heated gas over an annular shroud surface . The blast waves are generated by laser radiation heating of air using Laser Supported Detonation ( LSD ) waves . The phenomenology of LSD waves is described , as is the ...
13. lappuse
... PRESSURE DRAG OF AIRFOILS BY INTEGRATION OF SURFACE PRESSURES William H. Phillips Oct. 1990 26 p ( NASA - TM - 102722 ; NAS 1.15 : 102722 ) Avail : NTIS HC / MF A03 CSCL 01C A study was conducted of the causes of pressure drag of ...
... PRESSURE DRAG OF AIRFOILS BY INTEGRATION OF SURFACE PRESSURES William H. Phillips Oct. 1990 26 p ( NASA - TM - 102722 ; NAS 1.15 : 102722 ) Avail : NTIS HC / MF A03 CSCL 01C A study was conducted of the causes of pressure drag of ...
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Citi izdevumi - Skatīt visu
Bieži izmantoti vārdi un frāzes
A17 CSCL Abstr aerodynamic aeroelastic Aeronautics and Space Aerospace AGARD AGARD/Scientific Publications Executive Air Traffic Handling airfoil algorithm alloys Ames Research Center analysis Atmospheric Author cirrus cirrus clouds cloud composite Computational Fluid Dynamics Contract Copyright Avail Dept described developed effects electron energy Engineering ENGLISH summary equations evaluation experimental field flow function grid Guidance of Aircraft HC/MF A03 CSCL heat Includes Inst interaction investigated Langley Research Center laser lidar magnetic measurements mechanical Meteorological Satellite Center method Microfilms Order NASA National Aeronautics National Lab Nationals requests available Navier-Stokes equations Netherlands Non-NATO Nationals requests nonlinear NTIS HC/MF A03 numerical observed operating optical parameters performance Ph.D plasma Plasma Physics Prediction presented primary document problems Propulsion Report Sandia National Labs simulation solar Space Administration spacecraft superconducting surface techniques Technology temperature thermal Thesis turbulence Univ Universiteit Twente velocity wave wind windshear
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