... METHOD FOR OPTIMIZATION OF THE LOWER PART OF AIRCRAFT WING PROFILE A.Prangishvili, T ... the new algorithm the problem of flow around of aircraft wing profile is presented ...
... The blanking can be extended for a duration longer than the basic radar pulse in order to also eliminate delayed reflections of the pulse from aircraft, etc. ...
... Superboom, or sonic boom focusing, occurs during certain manoeuvres (sharp turns, low Mach flight, acceleration) of the aircraft, leading to amplification of ground pressures up to 2 to 5 times the primary boom. ...
... DRIVER: Numerical investigation of aerodynamic and aeroacoustic charateristics of bluff aircraft elements and complex turbulent flows, design of better noise prediction tools for development of quieter aircrafts . ...
... Equation in a Hilb ert Space A. V. Balakrishnan UCLA Department of Electrical Engineering, Los Angeles CA 90095-1594, U.S.A. e-mail: bal@ee.ucla.edu Flutter is an endemic instability of all aircraft that occurs at highenough speed at any altitude ...
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Ссылки http://pont2008.cs.msu.ru/files/en/abstracts/Balakrishnan.pdf -- 34.9 Кб -- 29.02.2008
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Ссылки http://pont2008.cmc.msu.ru/files/en/abstracts/Balakrishnan.pdf -- 34.9 Кб -- 29.02.2008 Похожие документы