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.
19. lappuse
... CSCL 21H A number of booster propulsion system concepts are being considered for the next generation of manned and unmanned space launch vehicles . The one propulsion system concept that has potential for reducing costs with increased ...
... CSCL 21H A number of booster propulsion system concepts are being considered for the next generation of manned and unmanned space launch vehicles . The one propulsion system concept that has potential for reducing costs with increased ...
20. lappuse
... CSCL 21H The purpose of the Integrated Hydrogen / Oxygen Technology ( IHOT ) study was to determine if the vehicle / mission needs and technology of the 1990's support development of an all cryogenic H2 / 02 system . In order to ...
... CSCL 21H The purpose of the Integrated Hydrogen / Oxygen Technology ( IHOT ) study was to determine if the vehicle / mission needs and technology of the 1990's support development of an all cryogenic H2 / 02 system . In order to ...
21. lappuse
... CSCL 11D Delamination in the form of cracking or separation between plies in an advanced fiber composite laminate is a problem of major concern . Both advanced analytical methods and advanced computational analyses are conducted to ...
... CSCL 11D Delamination in the form of cracking or separation between plies in an advanced fiber composite laminate is a problem of major concern . Both advanced analytical methods and advanced computational analyses are conducted to ...
51. lappuse
... CSCL 20K The purpose of this work - in - progress is to present a semi - empirical analysis method developed to predict the buckling and crippling loads of carbon / epoxy fabric blade stiffened panels in compression . This is a hand ...
... CSCL 20K The purpose of this work - in - progress is to present a semi - empirical analysis method developed to predict the buckling and crippling loads of carbon / epoxy fabric blade stiffened panels in compression . This is a hand ...
52. lappuse
... CSCL 20K The objective is to demonstrate discrete extremum methods of structural analysis as a tool for structural system reliability evaluation . Specifically , linear and multiobjective linear pro- gramming models for analysis of ...
... CSCL 20K The objective is to demonstrate discrete extremum methods of structural analysis as a tool for structural system reliability evaluation . Specifically , linear and multiobjective linear pro- gramming models for analysis of ...
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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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