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.
8. lappuse
... simulation technology . For related information see also 18 Spacecraft Design , Testing and Performance and 39 Structural Mechanics . For land transportation vehicles see 85 Urban Technology and Transportation . 06 AIRCRAFT ...
... simulation technology . For related information see also 18 Spacecraft Design , Testing and Performance and 39 Structural Mechanics . For land transportation vehicles see 85 Urban Technology and Transportation . 06 AIRCRAFT ...
3. lappuse
... simulation , this local peak heating has been analyzed for the three space plane configurations proposed by the National Aerospace Laboratory ( NAL ) . The proposed models have different wing leading edge sweep angles , and effects of ...
... simulation , this local peak heating has been analyzed for the three space plane configurations proposed by the National Aerospace Laboratory ( NAL ) . The proposed models have different wing leading edge sweep angles , and effects of ...
5. lappuse
... simulated iteratively using a surface transpiration model . A comparison with experimental results shows that the ... simulation makes use of a simple algebraic turbulence model . Using a sharp leading edge delta wing , the influence ...
... simulated iteratively using a surface transpiration model . A comparison with experimental results shows that the ... simulation makes use of a simple algebraic turbulence model . Using a sharp leading edge delta wing , the influence ...
11. lappuse
... simulation of the ERH thruster is accomplished with a one - dimensional model of blast waves propagating uniformly and radially outward from a laser - generated line source of high pressure , high temperature gas . Cylindrical blast ...
... simulation of the ERH thruster is accomplished with a one - dimensional model of blast waves propagating uniformly and radially outward from a laser - generated line source of high pressure , high temperature gas . Cylindrical blast ...
13. lappuse
... simulation control unit , the visual simulation unit and the motion simulation unit over a period of three years and four months since 1980. The present report explains the configuration , function , and capacity of the motion simulation ...
... simulation control unit , the visual simulation unit and the motion simulation unit over a period of three years and four months since 1980. The present report explains the configuration , function , and capacity of the motion simulation ...
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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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