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Friday, May 15, 2020 | History

2 edition of Theoretical and experimental engine-inlet flow fields for fighter forebodies found in the catalog.

Theoretical and experimental engine-inlet flow fields for fighter forebodies

Steven F. Yaros

Theoretical and experimental engine-inlet flow fields for fighter forebodies

by Steven F. Yaros

  • 119 Want to read
  • 5 Currently reading

Published by National Aeronautics and Space Administration, Scientific and Technical Information Branch, For sale by the National Technical Information Service] in Washington, D.C, [Springfield, Va .
Written in English

    Subjects:
  • Fighter planes.,
  • Aerodynamics, Supersonic.,
  • Aerodynamics, Transonic.

  • Edition Notes

    StatementSteven F. Yaros.
    SeriesNASA technical paper -- 2270.
    ContributionsUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
    The Physical Object
    Pagination63 p. :
    Number of Pages63
    ID Numbers
    Open LibraryOL17663544M

    The Application of Computational Fluid Dynamic Analysis to Jet Engine Inlet Flow Quality. Undergraduate Honors Thesis. Presented in Partial Fulfillment of the Requirements for. Graduation with Honors Research Distinction. in the Department of Mechanical and Aerospace Engineering at. The Ohio State University. By. Ryan W. Winfree. Kim. G. T. Experimental Study on Free Jet Flow with Applied electric Fields th. ICDERS – August , - Leeds 3. 3 Experiment. Fig 2. Schematic of experimental set up. The experimental apparatus consisted of a nozzle, gas supply systems, an oscilloscope, an amplifier.

    A theory for base pressures in transonic and supersonic flow / (Urbana, Ill.: Mechanical Engineering Dept., Univ. of Illinois, ), by Helmut Hans Korst, M. E. Childs, R. H. Page, and University of Illinois (Urbana-Champaign campus). Engineering Experiment Station (page images at . The study of fluid mechanics is fundamental to modern applied mathematics, with applications to oceans, the atmosphere, flow in pipes, aircraft, blood flow and very much more. This text provides an introduction to the mathematical approach to this subject and to many of its main ideas, based on material typically found in most university courses/5(33).

    Could such a book ever be made I was being "exposed" to the wonders and evils of Fs, Fs and F-4s during my military service in the eastern part of Turkey during turbulent times. This book is filled with knowledge on almost each and every model of fighter aircraft which ever had any significance, beginning from the early 20th century.4/5. Analytical and experimental study of flow through an axial turbine stage with a nonuniform inlet radial temperature profile. Aircraft engine inlet pressure distortion testing in a ground test facility. Analytical characterization of flow fields in side-inlet dump combustors.


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Theoretical and experimental engine-inlet flow fields for fighter forebodies by Steven F. Yaros Download PDF EPUB FB2

Get this from a library. Theoretical and experimental engine-inlet flow fields for fighter forebodies. [Steven F Yaros; United States.

National Aeronautics and Space Administration. Scientific and Technical Information Branch.]. The capability of two numerical methods, one for transonic and one for supersonic flows, to predict the flow fields about representative fighter aircraft forebodies in the vicinity of the engine inlets was examined.

The Mach number range covered was to and the. The capability of two numerical methods, one for transonic and one for supersonic flows, to predict the flow fields about representative fighter aircraft forebodies in the vicinity of the engine inlets was examined.

The Mach number range covered was to and the Author: S. Yaros. Theoretical and experimental engine-inlet flow fields for fighter forebodies / By Steven F.

Yaros and United States. National Aeronautics and Space Administration. February \. - NASA TP i I c.1 i I Steven F. 'Yaros '. Theoretical and Experimental Engine-Inlet Flow Fields for Fighter Forebodies Steven F.

Yaros Langley Research Center Hampton, Virginia. a INTRODUCTION. Modeling and Identification of Large Sideslip Effects from Flight Experiments Theoretical and experimental engine-inlet flow fields for fighter forebodies to predict the flow fields about.

The flow circulation is found to well couple the inlet velocity and the flow guide angle as Γ = π D d u a sin θ. The results have also shown that the JFRFF has a larger flame height than the free jet fire in still air, while the lift-off height is shorter than the free jet by: 1.

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