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
... solutions of the equations of HSDT . Detailed discussions are found for example in papers by Cole , Mirels , Chernyi ... solution of the flow field for any k greater than 2/3 is given . The effect of varying k on C sub L sup 3/2 C sub D ...
... solutions of the equations of HSDT . Detailed discussions are found for example in papers by Cole , Mirels , Chernyi ... solution of the flow field for any k greater than 2/3 is given . The effect of varying k on C sub L sup 3/2 C sub D ...
3. lappuse
... solution algorithm . Numerical computations were carried out at M ( sub infinity ) = 7.0 and Reynolds number of 4.4 x 10 ( exp 6 ) at angles of attack alpha = 0 , 10 , and 20 deg . Numerical results are compared with experimental heat ...
... solution algorithm . Numerical computations were carried out at M ( sub infinity ) = 7.0 and Reynolds number of 4.4 x 10 ( exp 6 ) at angles of attack alpha = 0 , 10 , and 20 deg . Numerical results are compared with experimental heat ...
5. lappuse
... solution is simulated iteratively using a surface transpiration model . A comparison with experimental results shows that the method predicts the trend of the boundary layer effect correctly , although underestimates its magnitude ...
... solution is simulated iteratively using a surface transpiration model . A comparison with experimental results shows that the method predicts the trend of the boundary layer effect correctly , although underestimates its magnitude ...
6. lappuse
... solution which overcomes the problem of specularity , and enables the standard Polaroid acoustic ranger with its standard electronics to accurately measure the range and direction to objects , is presented . To support this assertion ...
... solution which overcomes the problem of specularity , and enables the standard Polaroid acoustic ranger with its standard electronics to accurately measure the range and direction to objects , is presented . To support this assertion ...
8. lappuse
... solution for the half - loop is poststall trajectory performing the half - loop in 13.6 seconds . The agility ... solutions of singular perturbation . Poststall solutions provide high turn rates but generate higher losses of energy than ...
... solution for the half - loop is poststall trajectory performing the half - loop in 13.6 seconds . The agility ... solutions of singular perturbation . Poststall solutions provide high turn rates but generate higher losses of energy than ...
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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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