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
... equations from the rotating to the nonrotating system . Similarly , the induced flow can be written in either the rotating or the nonrotating system . The effect of periodic coefficients is dependent upon which set of blade equations is ...
... equations from the rotating to the nonrotating system . Similarly , the induced flow can be written in either the rotating or the nonrotating system . The effect of periodic coefficients is dependent upon which set of blade equations is ...
3. lappuse
... equations in a finite volume formulation . An implicit approximately factored ADI method has been used as the solution algorithm . Numerical computations were carried out at M ( sub infinity ) = 7.0 and Reynolds number of 4.4 x 10 ( exp ...
... equations in a finite volume formulation . An implicit approximately factored ADI method has been used as the solution algorithm . Numerical computations were carried out at M ( sub infinity ) = 7.0 and Reynolds number of 4.4 x 10 ( exp ...
4. lappuse
... equation developed from the turbulent kinetic energy equation . The performance of the present code was evaluated by solving the flow around three airfoils using the Reynolds time - averaged Navier - Stokes equations . Excellent results ...
... equation developed from the turbulent kinetic energy equation . The performance of the present code was evaluated by solving the flow around three airfoils using the Reynolds time - averaged Navier - Stokes equations . Excellent results ...
7. lappuse
... equations . Their most salient feature , however , is that entities corresponding to components and interactions in the physical system are explicitly represented in the bond graph model , thus permitting systematic model updates to ...
... equations . Their most salient feature , however , is that entities corresponding to components and interactions in the physical system are explicitly represented in the bond graph model , thus permitting systematic model updates to ...
8. lappuse
... equations of motion and is based on both moment and force equations . The maximum principle solution for the half - loop is poststall trajectory performing the half - loop in 13.6 seconds . The agility induced by thrust vectoring ...
... equations of motion and is based on both moment and force equations . The maximum principle solution for the half - loop is poststall trajectory performing the half - loop in 13.6 seconds . The agility induced by thrust vectoring ...
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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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