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  1. 1
    Tandem air propellers.
    Published 1939
    Electronic resource (PDF)
    Government Document eBook
  2. 2
    Comparison of profile-drag and boundary℗--layer measurements obtained in flight and in the full℗--scale wind tunnel.
    Published 1939
    Electronic resource (PDF)
    Government Document eBook
  3. 3
    An experimental investigation of the normal acceleration of an airplane model in a gust.
    Published 1939
    Electronic resource (PDF)
    Government Document eBook
  4. 4
    Tests in the gust tunnel of a model of the XBM-1 airplane.
    Published 1939
    Electronic resource (PDF)
    Government Document eBook
  5. 5
    The 5- by 7-meter wind tunnel of the DVL.
    Published 1936
    Electronic resource (PDF)
    Government Document eBook
  6. 6
    Circulation measurements about tip of airfoil during flight through gust.
    Published 1939
    Electronic resource (PDF)
    Government Document eBook
  7. 7
    Free-spinning wind-tunnel tests of low-wing monoplane with systematic changes in wings and tails : 2. Mass distributed along fuselage.
    Published 1937
    Electronic resource (PDF)
    Government Document eBook
  8. 8
    Wind-tunnel tests of carburetor-intake rams.
    Published 1938
    Electronic resource (PDF)
    Government Document eBook
  9. 9
    Estimation of rate of change of yawing moment with sideslip.
    Published 1938
    Electronic resource (PDF)
    Government Document eBook
  10. 10
    Interference of wing and fuselage from tests of 17 combinations in N. A. C. A. variable-density tunnel combinations with special juncture.
    Published 1938
    Electronic resource (PDF)
    Government Document eBook
  11. 11
    Wind-tunnel tests of 2-engine airplane model as preliminary study of flight conditions arising on failure of one engine.
    Published 1938
    Electronic resource (PDF)
    Government Document eBook
  12. 12
    Wind℗-tunnel investigation of rectangular and tapered N. A. C. A. 23012 wings with plain ailerons and full℗-span split flaps.
    Published 1938
    Electronic resource (PDF)
    Government Document eBook
  13. 13
    Effects of partial-span plain flaps on aerodynamic characteristics of rectangular and tapered Clark Y wing.
    Published 1938
    Electronic resource (PDF)
    Government Document eBook
  14. 14
    Free-spinning wind-tunnel tests of low-wing monoplane with systematic changes in wings and tails, III. Mass distributed along the wings.
    Published 1938
    Electronic resource (PDF)
    Government Document eBook
  15. 15
    Tests of N-85, N-86, and N-87 airfoil sections in 11-inch high-speed wind tunnel.
    Published 1938
    Electronic resource (PDF)
    Government Document eBook
  16. 16
    Thrust anemometer measurements of wind velocity fluctuations, spectra and stress over the sea /
    by Smith, S. D.
    Published 1966
    Thesis Book
  17. 17
    A three component thrust anemometer for studies of vertical transports above the sea surface /
    by Doe, L. A. E.
    Published 1963
    Thesis Book
  18. 18
    The synoptic (A) scale circulations during the second phase of Gate 17 July-19 August 1974 /
    by Sadler, James C.
    Published 1979
    Book
  19. 19
    United States Coast Pilot : Atlantic Coast, Section A; St. Croix River to Cape Cod, Third edition, 1933.
    Published 1933
    Electronic resource (PDF)
    Government Document eBook
  20. 20
    A simplified theory of long waves on a baroclinic westerly current /
    by Hess, Seymour L.
    Published 1958
    Book
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