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
... regions of flow - field . Mesh generation is based on a locally mapped Delaunay technique in order to generate unstructured meshes with highly - stretched elements in the viscous regions . The flow equations are discretized using a ...
... regions of flow - field . Mesh generation is based on a locally mapped Delaunay technique in order to generate unstructured meshes with highly - stretched elements in the viscous regions . The flow equations are discretized using a ...
4. lappuse
... regions . The influence of history effects are described by an ordinary differential equation developed from the turbulent kinetic energy equation . The performance of the present code was evaluated by solving the flow around three ...
... regions . The influence of history effects are described by an ordinary differential equation developed from the turbulent kinetic energy equation . The performance of the present code was evaluated by solving the flow around three ...
5. lappuse
... REGION OF BODIES WITH CIRCULAR CROSS SECTION AT ANGLE OF ATTACK Helmut Esch 15 Mar. 1990 63 p In GERMAN ; ENGLISH summary Report will also be announced as translation ( ESA - TT - 1226 ) ( DLR - FB - 90-15 ; ISSN - 0171-1342 ; ETN - 90 ...
... REGION OF BODIES WITH CIRCULAR CROSS SECTION AT ANGLE OF ATTACK Helmut Esch 15 Mar. 1990 63 p In GERMAN ; ENGLISH summary Report will also be announced as translation ( ESA - TT - 1226 ) ( DLR - FB - 90-15 ; ISSN - 0171-1342 ; ETN - 90 ...
10. lappuse
... region caused by the coolant injection . NASDA N91-10061 * # Ohio State Univ . , Columbus . Dept. of Aeronautical and Astronautical Engineering . SUPERSONIC COMBUSTION ENGINE TESTBED , HEAT LIGHTNING Final Report D. Hoying , C. Kelble ...
... region caused by the coolant injection . NASDA N91-10061 * # Ohio State Univ . , Columbus . Dept. of Aeronautical and Astronautical Engineering . SUPERSONIC COMBUSTION ENGINE TESTBED , HEAT LIGHTNING Final Report D. Hoying , C. Kelble ...
40. lappuse
... regions of the mesh , compares values of a variable of a given problem at selected times , compares values of a variable at selected times between problems for parameter studies , calculates derivatives of a variable with respect to ...
... regions of the mesh , compares values of a variable of a given problem at selected times , compares values of a variable at selected times between problems for parameter studies , calculates derivatives of a variable with respect to ...
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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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