Study of aerodynamic technology for single-cruise-engine V/STOL fighter/attack aircraft

phase I, final report

Publisher: National Aeronautics and Space Administration, Ames Research Center in Moffett Field, Calif

Written in English
Published: Downloads: 230
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Subjects:

  • Vertically rising aircraft -- Aerodynamics.,
  • Fighter planes -- Turbojet engines.

Edition Notes

StatementW.H. Foley, A.E. Sheridan, C.W. Smith ; prepared for Ames Research Center.
SeriesNASA contractor report -- NASA CR-166268.
ContributionsSheridan, A. E., Smith, C. W. 1943-, Ames Research Center., General Dynamics Corporation.
The Physical Object
FormatMicroform
Pagination1 v.
ID Numbers
Open LibraryOL17831482M

Study of aerodynamic technology for single-cruise-engine V/STOL fighter/attack aircraft Download PDF EPUB FB2

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[J R Hess; R L Bear; Ames Research Center.; McDonnell Company.]. Audio Books & Poetry Community Audio Computers & Technology Music, Arts & Culture News & Public Affairs Non-English Audio Spirituality & Religion.

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Due to the need to contain the spread of coronavirus (COVID) the Library building and reading rooms are closed to visitors until further notice. Investigation of the response to random wind gusts of a typical subsonic fighter aircraft in level flight with Mach number at sea Study of aerodynamic technology for single-cruise-engine V/STOL fighter/attack aircraft phase The additional thrust required to give an aircraft V/STOL capability may be obtained by diverting the engine exhaust flow through a thrust augmenting ejector.

Entrainment by the primary jet induces a flow of air through the ejector duct, thereby increasing the thrust of the by: RAF British Aerospace Harrier GR3 V/STOL jump-jet fighter | Flickr V/Stol Fighter (, MSX, MSX2, Mirrorsoft) | Releases 3/ PUB DORNIER V/STOL DO 31 E3 AIRCRAFT FLUGZEUG ORIGINAL A Brief History of V/STOL Combat Aircraft – Part IV: The Joint PDF] Study of aerodynamic technology for single-cruise-engine V.

A technique for determining wind tunnel wall effects for complex models using the low-order, three dimensional panel method PMARC (Panel Method Ames Research Center) has been developed.

Journal of Aircr J. HESS and R. BEAR Study of aerodynamic technology for single-cruise-engine V/STOL fighter/attack aircraft. NASA Contractor Report R. WOOD et al. Status review of a supersonically biased fighter wing design study. Journal of Cited by: Achetez et téléchargez ebook Study of aerodynamic technology for single-cruise-engine V/STOL fighter/attack aircraft (English Edition): Boutique Kindle - Science: Study of aerodynamic technology for single-cruise-engine V/STOL fighter/attack aircraft (English Edition) eBook: National Aeronautics and Space Administration NASA: : Kindle-ShopFormat: Kindle.

Advanced fighter technology integration (AFTI)/F Automated Maneuvering Attack System final flight test results. NASA Technical Reports Server (NTRS) Dowden, Donald J.; Bessette. Flight directors for STOl aircraft.

NASA Technical Reports Server (NTRS) Rabin, U. Flight director logic for flight path and airspeed control of a powered-lift STOL. PAN AIR results for Mach numbers of, and at angles of attack of 0, 5, and 10 were compared with data obtained in the Ames by Foot Transonic Wind Tunnel, at a Reynolds number of x 10 6 based on c.

INTRODUCTION A jointly sponsored NASA Ames and Navy program was initiated in to develop aerodyn,unic technology for post. Then, in Fighter Aircraft: W.P.

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