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
... approach , a flux split upwind TVD scheme was adopted by using thin layer Navier - Stokes equations in a finite volume formulation . An implicit approximately factored ADI method has been used as the solution algorithm . Numerical ...
... approach , a flux split upwind TVD scheme was adopted by using thin layer Navier - Stokes equations in a finite volume formulation . An implicit approximately factored ADI method has been used as the solution algorithm . Numerical ...
6. lappuse
... 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 . This system is composed of eight - light units arranged in a line perpendicular ...
... 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 . This system is composed of eight - light units arranged in a line perpendicular ...
9. lappuse
... approach utilized by the design team , the AAAI Program has elected to create an Industry Liaison Section ( ILS ) to ... approaches are considered in isotropic , organic composite , and metal matrix composite materials ; structural ...
... approach utilized by the design team , the AAAI Program has elected to create an Industry Liaison Section ( ILS ) to ... approaches are considered in isotropic , organic composite , and metal matrix composite materials ; structural ...
18. lappuse
... approach , compressive pre - stress is placed in the liner such that it will not separate from the overwrap . A finite element program is used to show stresses in the liner and overwrap for various tank pressures for the pre - stressed ...
... approach , compressive pre - stress is placed in the liner such that it will not separate from the overwrap . A finite element program is used to show stresses in the liner and overwrap for various tank pressures for the pre - stressed ...
20. lappuse
... approach of designing Integrated Auxiliary Propulsion Systems ( IAPS ) for a representative manned vehicle ; the ... approaches . The IHOT study resulted in the definition of three APS concepts ; two cryogenic IAPS , and a third concept ...
... approach of designing Integrated Auxiliary Propulsion Systems ( IAPS ) for a representative manned vehicle ; the ... approaches . The IHOT study resulted in the definition of three APS concepts ; two cryogenic IAPS , and a third concept ...
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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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