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
... WAVES B. A. Wagner 1990 10 p Presented at the 1st International Hypersonic Waverider Symposium , College Park , MD , Oct. 1990 ( Contract W - 7405 - eng - 36 ) ( DE90-014903 ; LA - UR - 90-2437 ; CONF - 9010154-1 ) Avail : NTIS HC / MF ...
... WAVES B. A. Wagner 1990 10 p Presented at the 1st International Hypersonic Waverider Symposium , College Park , MD , Oct. 1990 ( Contract W - 7405 - eng - 36 ) ( DE90-014903 ; LA - UR - 90-2437 ; CONF - 9010154-1 ) Avail : NTIS HC / MF ...
7. lappuse
... wave drag . The leading edge and lower surface of a waverider was mapped out from a known flow field and optimized for cruising at Mach 6 and at high altitudes . The shockwave generated by a waverider remains attached along the entire ...
... wave drag . The leading edge and lower surface of a waverider was mapped out from a known flow field and optimized for cruising at Mach 6 and at high altitudes . The shockwave generated by a waverider remains attached along the entire ...
11. lappuse
... waves propagating uniformly and radially outward from a laser - generated line source of high pressure , high temperature gas . Cylindrical blast wave scaling relationships developed by Sedov are employed in this model . The possibility ...
... waves propagating uniformly and radially outward from a laser - generated line source of high pressure , high temperature gas . Cylindrical blast wave scaling relationships developed by Sedov are employed in this model . The possibility ...
12. lappuse
... wave drag . The need to consider 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 ...
... wave drag . The need to consider 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 ...
21. lappuse
... waves are presented in Part 2. Preliminary results indicated that the leaky Lamb - wave technique appeared to be the most promising NDE tool for characterizing the level of heat damage in IM6 / 3501-6 laminates . This technique is ...
... waves are presented in Part 2. Preliminary results indicated that the leaky Lamb - wave technique appeared to be the most promising NDE tool for characterizing the level of heat damage in IM6 / 3501-6 laminates . This technique is ...
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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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