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
... experimental heat transfer measurements by the infrared system developed in the hypersonic wind tunnel ( HWT ) at NAL . Author N91-10012 # National Aerospace Lab . , Tokyo ( Japan ) . Aerodynamics Div . COMPARISON BETWEEN THE NULL ...
... experimental heat transfer measurements by the infrared system developed in the hypersonic wind tunnel ( HWT ) at NAL . Author N91-10012 # National Aerospace Lab . , Tokyo ( Japan ) . Aerodynamics Div . COMPARISON BETWEEN THE NULL ...
4. lappuse
... experimental data , it is concluded that the present code in conjunction with the new nonequilibrium turbulence model gives excellent results . Author N91-10020 * # National Aeronautics and Space Administration . Langley Research Center ...
... experimental data , it is concluded that the present code in conjunction with the new nonequilibrium turbulence model gives excellent results . Author N91-10020 * # National Aeronautics and Space Administration . Langley Research Center ...
5. lappuse
... experimental results shows that the method predicts the trend of the boundary layer effect correctly , although underestimates its magnitude . Author N91-10024 # Helsinki Univ . Technology , Otaniemi ( Finland ) . Aerodynamics Lab ...
... experimental results shows that the method predicts the trend of the boundary layer effect correctly , although underestimates its magnitude . Author N91-10024 # Helsinki Univ . Technology , Otaniemi ( Finland ) . Aerodynamics Lab ...
6. lappuse
... 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 guidance aid both STOL and CTOL landings ...
... 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 guidance aid both STOL and CTOL landings ...
7. lappuse
... experimental STOL craft . Prior to application to the experimental craft , a development technology test was carried out on the parts other than the C - 1 common parts of these actuators . The test was composed of a function and ...
... experimental STOL craft . Prior to application to the experimental craft , a development technology test was carried out on the parts other than the C - 1 common parts of these actuators . The test was composed of a function and ...
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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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