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.
10. lappuse
... method is presented for calculating the quasi - steady transonic flow over a lifting or non - lifting rotor blade in both hover and forward flight by using Euler equations . The approach is to solve Euler equations in a rotor - fixed ...
... method is presented for calculating the quasi - steady transonic flow over a lifting or non - lifting rotor blade in both hover and forward flight by using Euler equations . The approach is to solve Euler equations in a rotor - fixed ...
10. lappuse
... method has been used as the solution algorithm . Numerical computations were carried out at M ( sub infinity ) = 7.0 ... method is stronger to the small number of simulation molecules than the TC method because of the accurate NC ...
... method has been used as the solution algorithm . Numerical computations were carried out at M ( sub infinity ) = 7.0 ... method is stronger to the small number of simulation molecules than the TC method because of the accurate NC ...
10. lappuse
... method for three - dimensional compressible laminar or turbulent flow is proposed . The resulting computer program is valid only for simple wings . The panel model may also contain body - like components , however . The friction drag of ...
... method for three - dimensional compressible laminar or turbulent flow is proposed . The resulting computer program is valid only for simple wings . The panel model may also contain body - like components , however . The friction drag of ...
10. lappuse
... method for using fast jet actuators for steering the angle of attack of projectiles is described . In order to minimize the reaction time the response to pulse commands is analyzed . The conditions for inducing an angle of attack along ...
... method for using fast jet actuators for steering the angle of attack of projectiles is described . In order to minimize the reaction time the response to pulse commands is analyzed . The conditions for inducing an angle of attack along ...
13. lappuse
... method , joint - motion suspension method , joint - motion support method , and special drive method . The joint - motion six - freedom - degree support method was adopted . NASDA N91-10081 National Aerospace Lab . , Tokyo ( Japan ) ...
... method , joint - motion suspension method , joint - motion support method , and special drive method . The joint - motion six - freedom - degree support method was adopted . NASDA N91-10081 National Aerospace Lab . , Tokyo ( Japan ) ...
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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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