Scientific and Technical Aerospace Reports, 24. sējums,21-24. izdevumsNASA, Office of Scientific and Technical Information, 1986 Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database. |
No grāmatas satura
1.–5. rezultāts no 100.
3263. lappuse
... EXPERIMENTAL AND THEORETICAL STUDY OF PROPELLER SPINNER / SHANK INTERFERENCE M.S. Thesis Carl Clayton Cornell May 1986 143 p ( Contract NAS3-272 ) ( NASA - CR - 176954 ; NAS 1.26 : 176954 ) HC A07 / MF A01 CSCL 01A Avail : NTIS A ...
... EXPERIMENTAL AND THEORETICAL STUDY OF PROPELLER SPINNER / SHANK INTERFERENCE M.S. Thesis Carl Clayton Cornell May 1986 143 p ( Contract NAS3-272 ) ( NASA - CR - 176954 ; NAS 1.26 : 176954 ) HC A07 / MF A01 CSCL 01A Avail : NTIS A ...
3264. lappuse
... experimental data . These comparisons showed that , in general , the calculated base pressures are greater than the experimental base pressures . This lack of agreement raises questions about the applicability of a single stream ...
... experimental data . These comparisons showed that , in general , the calculated base pressures are greater than the experimental base pressures . This lack of agreement raises questions about the applicability of a single stream ...
3271. lappuse
... experiment verified the existence of the second solution ejector flow , where the flow after complete mixing is supersonic . Thrust augmentation in excess of 1.2 was demonstrated for both hot and cold primary jets . The experimental ...
... experiment verified the existence of the second solution ejector flow , where the flow after complete mixing is supersonic . Thrust augmentation in excess of 1.2 was demonstrated for both hot and cold primary jets . The experimental ...
3271. lappuse
... experiment verified the existence of the second solution ejector flow , where the flow after complete mixing is supersonic . Thrust augmentation in excess of 1.2 was demonstrated for both hot and cold primary jets . The experimental ...
... experiment verified the existence of the second solution ejector flow , where the flow after complete mixing is supersonic . Thrust augmentation in excess of 1.2 was demonstrated for both hot and cold primary jets . The experimental ...
3272. lappuse
... experimental study of local and mean heat transfer over the leading and trailing surfaces of a square - sectioned duct which is constrained to rotate about an axis perpendicular to the main direction of through flow are described . Both ...
... experimental study of local and mean heat transfer over the leading and trailing surfaces of a square - sectioned duct which is constrained to rotate about an axis perpendicular to the main direction of through flow are described . Both ...
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A01 Avail A01 CSCL aerodynamic Aeronautics and Space Aerospace AGARD Heat Transfer Air Force aircraft algorithm analysis applications Author blade Boston Spa Calif Collection of Micrometeoroids Contract Cooling in Gas cosmic dust CSCL 03B Dept discussed dynamic effects electron energy Engineering equations evaluation experimental Final Report flight flow fuel function Gas Turbines Sep Includes investigated Langley Research Center laser Lewis Research Center linear Lunar and Planetary materials measurements mechanical metal method Micrometeoroids NASA National Aeronautics National Lab nonlinear NTIS HC A02/MF operation optical parameters particles Patent physical Planetary Inst prediction presented pressure primary document problem radiation related information rotor Sandia National Labs Science simulation solar Space Administration Space Station 1986 spacecraft Spacecraft Propulsion structure surface techniques temperature thermal tion Transfer and Cooling Transl turbulence Univ West Germany Wright-Patterson AFB