Scientific and Technical Aerospace Reports, 29. sējumsScientific and Technical Information Branch, National Aeronautics and Space Administration, 1991 |
No grāmatas satura
1.5. rezultāts no 100.
9. lappuse
... integrated circuitry . For related information see also 60 Computer Operations and Hardware and 76 Solid - State Physics . 34 FLUID MECHANICS AND HEAT TRANSFER 39 Includes boundary layers ; hydrodynamics ; fluidics ; mass transfer and ...
... integrated circuitry . For related information see also 60 Computer Operations and Hardware and 76 Solid - State Physics . 34 FLUID MECHANICS AND HEAT TRANSFER 39 Includes boundary layers ; hydrodynamics ; fluidics ; mass transfer and ...
10. lappuse
... Integrated Technology A 153W airfoil . Based on the comparison of the numerical solutions with the available ... integration with the governing flow equations . Calculations were performed using the Euler equations to verify the ...
... Integrated Technology A 153W airfoil . Based on the comparison of the numerical solutions with the available ... integration with the governing flow equations . Calculations were performed using the Euler equations to verify the ...
12. lappuse
... integrated rather than isolated installations is emphasized . ESA N91-10072 # Rolls - Royce Ltd. , Bristol ( England ) . APPLICATIONS OF THERMALLY SPRAYED COATING SYSTEMS IN AERO ENGINES T. N. Rhys - Jones Derby , England 15 Sep. 1989 ...
... integrated rather than isolated installations is emphasized . ESA N91-10072 # Rolls - Royce Ltd. , Bristol ( England ) . APPLICATIONS OF THERMALLY SPRAYED COATING SYSTEMS IN AERO ENGINES T. N. Rhys - Jones Derby , England 15 Sep. 1989 ...
13. lappuse
... integration of surface friction along the chord . Herein , the pressure drag is obtained by integrating the streamwise components of surface pressure around the airfoil . Studies were made to verify the accuracy of the integration ...
... integration of surface friction along the chord . Herein , the pressure drag is obtained by integrating the streamwise components of surface pressure around the airfoil . Studies were made to verify the accuracy of the integration ...
17. lappuse
... integrated test ( SIT ) conducted from July 30 , 1989 , through August 11 , 1989 , tested an integrated air revitalization system . During this test , the trace contaminant control subsystem ( TCCS ) was directly integrated with the ...
... integrated test ( SIT ) conducted from July 30 , 1989 , through August 11 , 1989 , tested an integrated air revitalization system . During this test , the trace contaminant control subsystem ( TCCS ) was directly integrated with the ...
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A03 CSCL Aeronautics and Space Aerospace aircraft algorithm analysis applications Atmospheric Author Center Technical Note cirrus clouds Computational Fluid Dynamics Contract Copyright Avail CSCL 04B density Dept developed Dutch guilders Dynamics effects electron energy Engineering ENGLISH summary equations field FIRE Science Results flow function GMS System HC/MF A17 CSCL Includes infrared Inst ISCCP Joint Publications Research JPRS Report Langley Research Center laser lidar magnetic materials measurements Meteorological Satellite Center method NASA National Aeronautics Netherlands nonlinear NTIS HC/MF A03 observed optical parameters particle Physics plasma Plasma Physics presented primary document problem Publications Research Service radiation Results 1988 Jul San Nicolas Island Sandia National Labs Satellite Center Technical Science Results 1988 simulation solar Space Administration spacecraft Special Issue 1989 structure summary For primary Summary of GMS superconducting surface techniques temperature tokamak Tokyo Japan turbulence Univ Universiteit Twente USSR wave
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