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.
2. lappuse
... compared to numerical computations based on two design codes and a Parabolized Navier - Stokes ( PNS ) code . The design codes , in general , gave good results . The PNS code complemented these results by providing more details on the ...
... compared to numerical computations based on two design codes and a Parabolized Navier - Stokes ( PNS ) code . The design codes , in general , gave good results . The PNS code complemented these results by providing more details on the ...
3. lappuse
... compared with 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 ...
... compared with 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 ...
4. lappuse
... compared with results found for a two bladed rotor in hovering and advancing flight . The comparison shows a good ... comparable with the boundary layer thickness so that a quasi - parallel approach to the instability problem can be ...
... compared with results found for a two bladed rotor in hovering and advancing flight . The comparison shows a good ... comparable with the boundary layer thickness so that a quasi - parallel approach to the instability problem can be ...
5. lappuse
... comparing the results to analytical solutions , experimental results , and other representative computations ... compared to validate the numerical method . The topological structure of the flow is interpreted . An explanation is ...
... comparing the results to analytical solutions , experimental results , and other representative computations ... compared to validate the numerical method . The topological structure of the flow is interpreted . An explanation is ...
6. lappuse
... compared . Some attempts were also made to estimate sensor noise parameters . NASDA N91-10032 # Federal Aviation Administration , Washington , DC . NATIONAL AIRSPACE SYSTEM : IN - FLIGHT ASSISTANCE OPERATIONAL CONCEPT 27 Jul . 1989 38 p ...
... compared . Some attempts were also made to estimate sensor noise parameters . NASDA N91-10032 # Federal Aviation Administration , Washington , DC . NATIONAL AIRSPACE SYSTEM : IN - FLIGHT ASSISTANCE OPERATIONAL CONCEPT 27 Jul . 1989 38 p ...
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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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