Langley Research Center

adj=on}} subsonic [[wind tunnel The Langley Research Center (LaRC or NASA Langley), located in Hampton, Virginia, near the Chesapeake Bay front of Langley Air Force Base, is the oldest of NASA's field centers. LaRC has focused primarily on aeronautical research but has also tested space hardware such as the Apollo Lunar Module. In addition, many of the earliest high-profile space missions were planned and designed on-site. Langley was also considered a potential site for NASA's Manned Spacecraft Center prior to the eventual selection of Houston, Texas.

Established in 1917 by the National Advisory Committee for Aeronautics (NACA), the research center devotes two-thirds of its programs to aeronautics and the rest to space. LaRC researchers use more than 40 wind tunnels to study and improve aircraft and spacecraft safety, performance, and efficiency. Between 1958 and 1963, when NASA (the successor agency to NACA) started Project Mercury, LaRC served as the main office of the Space Task Group.

In September 2019, after previously serving as associate director and deputy director, Clayton P. Turner was appointed director of NASA Langley. Provided by Wikipedia
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  1. 1

    A study of the application of heat or force fields to the sonic-boom-minimization problem / by Miller, David S. (Of Langley Research Center)

    Published 1969
    Government Document Book
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    Lee-side flow over delta wings at supersonic speeds / by Miller, David S. (Of Langley Research Center), Wood, Richard M.

    Published 1985
    “…Langley Research Center…”
    Online Access
    Government Document eBook
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    Numerical methods for the design and analysis of wings at supersonic speeds by Carlson, Harry W.

    Published 1974
    Other Authors: “…David S. (Of Langley Research Center)…”
    Government Document Book
  8. 8

    Wing planform effects at supersonic speeds for an advanced fighter configuration / by Wood, Richard M.

    Published 1984
    Other Authors: “…David S. (Of Langley Research Center)…”
    Search for the full-text version of this title in HathiTrust
    Government Document Book
  9. 9

    Experimental investigation of leading-edge thrust at supersonic speeds / by Wood, Richard M.

    Published 1983
    Other Authors: “…David S. (Of Langley Research Center)…”
    Search for the full-text version of this title in HathiTrust
    Government Document Book
  10. 10

    Pressure and force data for a flat wing and a warped conical wing having a shockless recompression at Mach 1.62 /

    Published 1981
    Other Authors: “…David S. (Of Langley Research Center)…”
    Search for the full-text version of this title in HathiTrust
    Government Document Book
  11. 11

    Effect of fuselage upwash on the supersonic longitudinal aerodynamic characteristics of two fighter configurations / by Wood, Richard M.

    Published 1984
    Other Authors: “…David S. (Of Langley Research Center)…”
    Search for the full-text version of this title in HathiTrust
    Government Document Book
  12. 12

    Numerical method for design of minimum-drag supersonic wing camber with constraints on pitching moment and surface deformation / by Sorrells, Russell B.

    Published 1972
    Other Authors: “…David S. (Of Langley Research Center)…”
    Government Document Book
  13. 13

    Aerodynamic characteristics at Mach numbers of 1.5, 1.8, and 2.0 of a blended wing-body configuration with and without integral canards / by Robins, A. Warner

    Published 1979
    Other Authors: “…David S. (Of Langley Research Center)…”
    Search for the full-text version of this title in HathiTrust
    Government Document Book
  14. 14

    Body and canard effects on an attached-flow maneuver wing at Mach 1.62 / by Pittman, Jimmy L.

    Published 1984
    Other Authors: “…David S. (Of Langley Research Center)…”
    Search for the full-text version of this title in HathiTrust
    Government Document Book
  15. 15

    A non-dissipative staggered fourth-order accurate explicit finite difference scheme for the time-domain Maxwell's equations by Yeffet, Amir

    Published 1999
    “…Langley Research Center…”
    Government Document Microfilm Book
  16. 16

    Investigation of a technique for measuring dynamic ground effect in a subsonic wind tunnel by Graves, Sharon S.

    Published 1999
    “…Langley Research Center…”
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    Government Document Microfilm Book
  17. 17

    Parallel implementation of the discontinuous Galerkin method by Baggag, Abdelkader

    Published 1999
    “…Langley Research Center…”
    view full text online
    Government Document Microfilm Book
  18. 18

    Parallelization of a multigrid incompressible viscous cavity flow solver using openMP by Roe, Kevin

    Published 1999
    “…Langley Research Center…”
    Click here to view full text online
    Government Document Microfilm Book
  19. 19

    Advances in composites technology by Tenney, Darrel R.

    Published 1985
    “…Langley Research Center…”
    Government Document Book
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    Cyclic cryogenic thermal-mechanical testing of an X-33/RLV liquid oxygen tank concept by Rivers, H. Kevin

    Published 1999
    “…Langley Research Center…”
    Government Document Microfilm Book
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