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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    Performance of a high-speed compression-ignition engine using multiple orifice fuel injection nozzles / by Spanogle, J. A.

    Published 1930
    “…Langley Aeronautical Laboratory…”
    Government Document Book
  3. 3

    Critical combinations of torsion and direct axial stress for thin-walled cylinders / by Batdorf, S. B.

    Published 1947
    “…Langley Aeronautical Laboratory…”
    Full Text (via Knovel)
    Government Document eBook
  4. 4

    Critical stress of thin-walled cylinders in torsion / by Batdorf, S. B., Stein, Manuel, Schildcrout, Murry

    Published 1947
    “…Langley Aeronautical Laboratory…”
    Full Text (via Knovel)
    Government Document eBook
  5. 5

    Some remarks on an approximate method of estimating the wave drag due to thickness at supersonic speeds of three-dimensional wings with arbitrary profile / by Margolis, Kenneth

    Published 1952
    “…Langley Aeronautical Laboratory…”
    Government Document Book
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    Effects of boundary-layer displacement and leading-edge bluntness on pressure distribution, skin friction, and heat transfer of bodies at hypersonic speeds / by Bertram, Mitchel H.

    Published 1958
    “…Langley Aeronautical Laboratory…”
    Government Document Book
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    Estimation of the maximum angle of sideslip for determination of vertical-tail loads in rolling maneuvers / by Stone, Ralph W., Jr

    Published 1952
    “…Langley Aeronautical Laboratory…”
    Government Document Book
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    Heat transfer and recovery temperatures on a sphere with laminar, transitional, and turbulent boundary layers at Mach numbers of 2.00 and 4.15 / by Beckwith, Ivan E.

    Published 1957
    “…Langley Aeronautical Laboratory…”
    Government Document Book
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    Pressure rise associated with shock-induced boundary-layer separation / by Love, Eugene S.

    Published 1955
    “…Langley Aeronautical Laboratory…”
    Government Document Book
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    Investigation at supersonic speeds of the variation with Reynolds number and Mach number of the total, base, and skin-friction drag of seven boattail bodies of revolution designed... by Bromm, August F.

    Published 1956
    “…Langley Aeronautical Laboratory…”
    Government Document Book
  14. 14

    On subsonic flow past a paraboloid of revolution / by Kaplan, Carl

    Published 1957
    “…Langley Aeronautical Laboratory…”
    Government Document Book
  15. 15

    Theoretical and experimental dynamic loads for a prismatic float having an angle of dead rise of 22.5 degrees / by Mayo, Wilbur L.

    Published 1945
    Government Document Book
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    Lag in pressure systems at extremely low pressures / by Davis, William T.

    Published 1958
    “…Langley Aeronautical Laboratory…”
    Government Document Book
  17. 17

    Mass transfer cooling near the stagnation point / by Roberts, Leonard

    Published 1958
    “…Langley Aeronautical Laboratory…”
    Government Document Book
  18. 18

    A theoretical study of stagnation-point ablation / by Roberts, Leonard

    Published 1958
    “…Langley Aeronautical Laboratory…”
    Government Document Book
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    Supersonic wave interference affecting stability / by Love, Eugene S.

    Published 1958
    “…Langley Aeronautical Laboratory…”
    Government Document Book
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    Determination of transient skin temperature of conical bodies during short-time, high-speed flight / by Lo, Hsu

    Published 1948
    Government Document Book
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