Scientific and Technical Aerospace ReportsScientific and Technical Information Office, National Aeronautics and Space Administration, 1985 |
No grāmatas satura
1.–5. rezultāts no 100.
. lappuse
... obtained without charge from the DOE Technical Information Center . Avail : Univ . Microfilms . Documents so indicated are dissertations selected from Dissertation Abstracts and are sold by University Microfilms as xerographic copy ( HC ) ...
... obtained without charge from the DOE Technical Information Center . Avail : Univ . Microfilms . Documents so indicated are dissertations selected from Dissertation Abstracts and are sold by University Microfilms as xerographic copy ( HC ) ...
6. lappuse
... obtained from these experiments are compared with data obtained from computations using a boundary element method which is a modification of Morino's theory . In order to confirm the starting points of the trailing vortex sheets on the ...
... obtained from these experiments are compared with data obtained from computations using a boundary element method which is a modification of Morino's theory . In order to confirm the starting points of the trailing vortex sheets on the ...
6. lappuse
... obtained for 9.5 % force and pressure models of a V / STOL fighter / attack aircraft configuration with top mounted ... obtained by applying the Kutta condition at the trailing edge . Results were compared with those obtained from a ...
... obtained for 9.5 % force and pressure models of a V / STOL fighter / attack aircraft configuration with top mounted ... obtained by applying the Kutta condition at the trailing edge . Results were compared with those obtained from a ...
6. lappuse
... obtained from linear theories . A superposition principal was derived whereby the unsteady lift and moment acting on a thin airfoil with small camber and small angle of attack and subject to a two - dimensional gust can be constructed ...
... obtained from linear theories . A superposition principal was derived whereby the unsteady lift and moment acting on a thin airfoil with small camber and small angle of attack and subject to a two - dimensional gust can be constructed ...
10. lappuse
... obtained in conducting the study . The study objectives were : ( 1 ) the evaluation of the performance of a sunlight readable multifunction switch using an x - y dot matrix light emitting diode ( LED ) array and incorporating tactile ...
... obtained in conducting the study . The study objectives were : ( 1 ) the evaluation of the performance of a sunlight readable multifunction switch using an x - y dot matrix light emitting diode ( LED ) array and incorporating tactile ...
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306. lappuse - Includes applications of space technology to urban problems; technology transfer; technology assessment; and surface and mass transportation. For related information see 03 Air Transportation and Safety, 16 Space Transportation, and 44 Energy Production and Conversion.
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324. lappuse - E03 19 SPACECRAFT INSTRUMENTATION For related information see also 06 Aircraft Instrumentation and 35 Instrumentation and Photography.
185. lappuse - Virginia Polytechnic Inst. and State Univ., Blacksburg. Dept. of Engineering Science and Mechanics.