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Saturday, July 25, 2020 | History

2 edition of Boundary-layer transition results from the F-16XL-2 supersonic laminar flow control experiment found in the catalog.

Boundary-layer transition results from the F-16XL-2 supersonic laminar flow control experiment

Laurie A. Marshall

Boundary-layer transition results from the F-16XL-2 supersonic laminar flow control experiment

by Laurie A. Marshall

  • 53 Want to read
  • 12 Currently reading

Published by National Aeronautics and Space Administration, Dryden Flight Research Center, Available from NASA Center for AeroSpace Information in Edwards, Calif, Hanover, Md .
Written in English

    Subjects:
  • Aerodynamics, Supersonic.,
  • Boundary layer.,
  • F-16 (Jet fighter plane),
  • Laminar flow.

  • Edition Notes

    StatementLaurie A. Marshall.
    SeriesNASA/TM -- 1999-209013, NASA technical memorandum -- 1999-209013.
    ContributionsHugh L. Dryden Flight Research Center., United States. National Aeronautics and Space Administration.
    The Physical Object
    Paginationiv, 48 p. :
    Number of Pages48
    ID Numbers
    Open LibraryOL20639543M

    The concept Design analysis represents the subject, aboutness, idea or notion of resources found in Houston Public Library. Libri Tedeschi. Acquista online i tuoi Libri Tedeschi di Physik & Astronomie su Libreria Universitaria: scopri sconti e offerte speciali! - Pagina

    One of these was the potential application of a supersonic laminar flow control (SLFC) capability to a highly swept, cranked-arrow wing. The concept was to come up with a flight dem- onstration that would reduce the technical risk of using SLFC technology in the design, development, and production of a High-Speed Civil Transport (HSCT).


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Boundary-layer transition results from the F-16XL-2 supersonic laminar flow control experiment by Laurie A. Marshall Download PDF EPUB FB2

Boundary-Layer Transition Results From the FXL-2 Supersonic Laminar Flow Control Experiment Laurie A. Marshall NASA Dryden Flight Research Center Edwards, California December National Aeronautics and Space Administration Dryden Flight Research Center Edwards, California File Size: 1MB.

SUMMARY OF TRANSITION RESULTS FROM THE FXL-2 SUPERSONIC LAMINAR FLOW CONTROL EXPERIMENT Laurie A. Marshall * NASA Dryden Flight Research Center Edwards, California ABSTRACT A variable-porosity suction glove has been flown on the FXL-2 aircraft to demonstrate the feasibility of this technology for the proposed High-Speed Civil by: Boundary-layer transition results from the FXL-2 supersonic laminar flow control experiment (SuDoc NAS ) [Marshall, Laurie A.] on *FREE* shipping on qualifying offers.

Boundary-layer transition results from the FXL-2 supersonic laminar flow Author: Laurie A. Marshall. Get this from a library. Boundary-layer transition results from the FXL-2 supersonic laminar flow control experiment.

[Laurie A Marshall; Hugh L. Dryden Flight Research Center.]. Boundary-Layer Transition Results From the FXL-2 Supersonic Laminar Flow Control Experiment Laurie A. Marshall NASA Dryden Flight Research Center Edwards, California National Aeronautics and Space Administration Dryden Flight Research Center Edwards, California December Boundary Layer Flow Control by an Array of Ramp-Shaped Vortex Generators (Paperback or Softback) by Nasa Technical Reports Server (Ntrs) and a great selection of related books, art and collectibles available now at Boundary-layer transition results from the FXL-2 supersonic laminar flow control experiment.

Edwards, Calif.: Hanover, MD: Springfield, VA: National Aeronautics and Space Administration, Dryden Flight Research Center ; NASA Center for AeroSpace Information [distributor] ; National Technical Information Service [distributor.

MLA Citation. Buy Boundary-layer transition results from the FXL-2 supersonic laminar flow control experiment (SuDoc NAS ) by Laurie A. Marshall (ISBN:) from Amazon's Book Store. Everyday low prices and free delivery on eligible : Laurie A. Marshall. 21st Century Collection of NASA and NACA Dryden Technical Reports: X-Plane, SR, Space Shuttle, Hypersonic Research, Fighter Planes (Two CD-ROM Set) [News, World Spaceflight] on *FREE* shipping on qualifying offers.

21st Century Collection of NASA and NACA Dryden Technical Reports: X-Plane, SR, Space Shuttle, Hypersonic ResearchPrice: $ Free 2-day shipping. Buy Boundary-Layer Transition Results from the Fxl-2 Supersonic Laminar Flow Control Experiment at Boundary-Layer Transition Results from the FXL-2 Supersonic Laminar Flow Control Experiment eBook: National Aeronautics and Space Administration NASA: : Kindle StoreAuthor: National Aeronautics and Space Administration NASA.

Laminar boundary layer in conditions of "natural" transition to turbulent flow [microform] / N.F. Polyakov National Aeronautics and Space Administration Washington, D.C Australian/Harvard Citation. Polyakov, N.

& United States. National Aeronautics and Space Administration. Request PDF | Direct Numerical Simulations of Instability-Wave Generation and Propagation in Supersonic Boundary Layers | Stringent requirements for component performance plus economic and.

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American Institute of Aeronautics and Astronautics Sunrise Valley Drive, Suite Reston, VA The viscous-inviscid coupling between the boundary layer and the inviscid flow is also addressed. The book has a large number of homework problems. Boundary-Layer Transition Results From the F. 21st Century Collection of NASA and NACA Dryden Technical Reports: X-Plane, SR, Space Shuttle, Hypersonic Research, Fighter Planes (Two CD-ROM Set): World Spaceflight News: Books - or: World Spaceflight News.

provide air for the engines. A problem is the boundary layer is quite thin so you might need to use quite large wings or lifting body to get sufficient air for the engines. This could wind up producing just as much drag as what you are trying to get rid of. Another problem is that according to this web page at low density conditions the.

Boundary-Layer Transition Results from the FXL-2 Supersonic Laminar Flow Control Experiment. NASA Technical Reports Server (NTRS) Marshall, Laurie A. A variable-porosity suction glove has been flown on the FXL-2 aircraft to demonstrate the feasibility of this technology for the proposed High-Speed Civil Transport (HSCT).

Noté /5. Retrouvez Boundary-Layer Transition Results from the FXL-2 Supersonic Laminar Flow Control Experiment et des millions de livres en stock sur Achetez neuf ou d'occasionFormat: Broché. SUPERSONIC SHEAR INSTABILITIES IN ASTROPHYSICAL BOUNDARY LAYERS.

SciTech Connect. Belyaev, Mikhail A.; Rafikov, Roman R., E-mail: [email protected] Disk.Boundary-Layer Transition Results from the FXL-2 Supersonic Laminar Flow Control Experiment (English Edition) eBook: National Aeronautics and Space Administration NASA: : Kindle-ShopFormat: Kindle.Boundary-Layer Transition Results from the FXL-2 Supersonic Laminar Flow Control Experiment | National Aeronautics and Space Administration NASA | ISBN: | Kostenloser Versand für alle Bücher mit Versand und Verkauf duch : Taschenbuch.