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
... calculating the hypersonic flow of an inviscid reacting gas over an axisymmetric or planar body . The thermochemical model allows for the finite - rate chemical relaxation of an arbitrary mixture of perfect gases and the coupling of ...
... calculating the hypersonic flow of an inviscid reacting gas over an axisymmetric or planar body . The thermochemical model allows for the finite - rate chemical relaxation of an arbitrary mixture of perfect gases and the coupling of ...
2. lappuse
... CALCULATION I - Chung Chang Jun . 1990 23 p ( NASA - TP - 2375 ; A - 86374 - Pt - 3 ; NAS 1.60 : 2375 ) Avail : NTIS ... CALCULATIONS USING UNSTRUCTURED AND ADAPTIVE MESHES Final Report Dimitri J. Mavriplis Sep. 1990 32 p Submitted for ...
... CALCULATION I - Chung Chang Jun . 1990 23 p ( NASA - TP - 2375 ; A - 86374 - Pt - 3 ; NAS 1.60 : 2375 ) Avail : NTIS ... CALCULATIONS USING UNSTRUCTURED AND ADAPTIVE MESHES Final Report Dimitri J. Mavriplis Sep. 1990 32 p Submitted for ...
3. lappuse
... calculations are given . The Ga AEED device is concluded to be of not good enough quality for fair comparison to the silicon AEED . ESA N91-10017 # Institut Franco - Allemand de Recherches , Saint - Louis ( France ) . MEASUREMENT OF AIR ...
... calculations are given . The Ga AEED device is concluded to be of not good enough quality for fair comparison to the silicon AEED . ESA N91-10017 # Institut Franco - Allemand de Recherches , Saint - Louis ( France ) . MEASUREMENT OF AIR ...
4. lappuse
... Calculations were performed using the Euler equations to verify the modifications to the code and as a first step toward aeroelastic analysis using the Navier - Stokes equations . Results are presented for the NACA 0012 airfoil and a 45 ...
... Calculations were performed using the Euler equations to verify the modifications to the code and as a first step toward aeroelastic analysis using the Navier - Stokes equations . Results are presented for the NACA 0012 airfoil and a 45 ...
5. lappuse
... CALCULATION OF THREE - DIMENSIONAL VISCOUS / INVISCID INTERACTION IN SUBSONIC FLOW Ziqiang Zhu , Seppo Laine , and ... calculations , which are carried out along chordwise strips of the wing . The surface transpiration approach is used ...
... CALCULATION OF THREE - DIMENSIONAL VISCOUS / INVISCID INTERACTION IN SUBSONIC FLOW Ziqiang Zhu , Seppo Laine , and ... calculations , which are carried out along chordwise strips of the wing . The surface transpiration approach is used ...
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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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