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.
3. lappuse
... NTIS HC / MF A03 The evaluation of hypersonic aerothermodynamic heating along the wing leading edge of the space plane is very important for preliminary aerothermal structural design , because severe local peak heating is caused there ...
... NTIS HC / MF A03 The evaluation of hypersonic aerothermodynamic heating along the wing leading edge of the space plane is very important for preliminary aerothermal structural design , because severe local peak heating is caused there ...
5. lappuse
... NTIS HC / MF A03 Coupling MBB low - order panel code for three - dimensional compressible subsonic potential flow and Stock's boundary layer method for three - dimensional compressible laminar or turbulent flow is proposed . The ...
... NTIS HC / MF A03 Coupling MBB low - order panel code for three - dimensional compressible subsonic potential flow and Stock's boundary layer method for three - dimensional compressible laminar or turbulent flow is proposed . The ...
6. lappuse
... NTIS HC / MF A03 Flight tests of NAL QSTOL experimental aircraft are being conducted at Gifu airfield . The PAPI ( Precision Approach Path Indicator ) system was placed at the left side of runway 28 at Gifu airfield as a visual approach ...
... NTIS HC / MF A03 Flight tests of NAL QSTOL experimental aircraft are being conducted at Gifu airfield . The PAPI ( Precision Approach Path Indicator ) system was placed at the left side of runway 28 at Gifu airfield as a visual approach ...
9. lappuse
... NTIS HC / MF A03 A method for using fast jet actuators for steering the angle of attack of projectiles is described . In order to minimize the reaction time the response to pulse commands is analyzed . The conditions for inducing an ...
... NTIS HC / MF A03 A method for using fast jet actuators for steering the angle of attack of projectiles is described . In order to minimize the reaction time the response to pulse commands is analyzed . The conditions for inducing an ...
10. lappuse
... NTIS HC / MF A03 Trial fabrication of a triaxial sensor system , in which alpha is the front angle and beta is the side angles , and performance of wind tunnel tests are presented . An experiment based on the two - dimensional vector ...
... NTIS HC / MF A03 Trial fabrication of a triaxial sensor system , in which alpha is the front angle and beta is the side angles , and performance of wind tunnel tests are presented . An experiment based on the two - dimensional vector ...
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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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