Showing 1 - 20 results of 27 for search 'Heaslet, M. A. (Maxwell Alfred), 1907-', query time: 0.09s Refine Results
  1. 1

    Three-dimensional transonic flow theory applied to slender wings and bodies / by Heaslet, M. A. (Maxwell Alfred), 1907-

    Published 1956
    Government Document Book
  2. 2

    Particular solutions for flows at Mach number 1 / by Heaslet, M. A. (Maxwell Alfred), 1907-

    Published 1956
    Government Document Book
  3. 3

    The calculation of pressure on slender airplanes in subsonic and supersonic flow / by Heaslet, M. A. (Maxwell Alfred), 1907-

    Published 1953
    Government Document Book
  4. 4

    The minimization of wave drag for wings and bodies with a given base area or volume / by Heaslet, M. A. (Maxwell Alfred), 1907-

    Published 1954
    Government Document Book
  5. 5

    Drag minimization for wings in supersonic flow, with various constraints / by Heaslet, M. A. (Maxwell Alfred), 1907-

    Published 1958
    Government Document Book
  6. 6
  7. 7

    Axially symmetric shapes with minimum wave drag / by Heaslet, M. A. (Maxwell Alfred), 1907-

    Published 1955
    Government Document Book
  8. 8

    Compressible potential flow with circulation about a circular cylinder / by Heaslet, M. A. (Maxwell Alfred), 1907-

    Published 1944
    Government Document Book
  9. 9

    Numerical predictions of radiative interchange between conducting fins with mutual irradiations / by Heaslet, M. A. (Maxwell Alfred), 1907-

    Published 1961
    Government Document Book
  10. 10

    Critical Mach numbers of thin airfoil sections with plain flaps / by Heaslet, M. A. (Maxwell Alfred), 1907-

    Published 1946
    Government Document Book
  11. 11

    Theoretical investigation of methods for computing drag from wake surveys at high subsonic speeds / by Heaslet, M. A. (Maxwell Alfred), 1907-

    Published 1945
    Government Document Book
  12. 12
  13. 13
  14. 14
  15. 15

    Linearized compressible-flow theory for sonic flight speeds / by Heaslet, M. A. (Maxwell Alfred), 1907-

    Published 1949
    Government Document Book
  16. 16

    Two-dimensional unstead lift problems in supersonic flight / by Heaslet, M. A. (Maxwell Alfred), 1907-

    Published 1948
    Government Document Book
  17. 17
  18. 18

    Elementary number theory / by Uspensky, J. V. (James Victor), 1883-1947, Heaslet, M. A. (Maxwell Alfred), 1907-

    Published 1939
    Book
  19. 19

    Generalized conical-flow fields in supersonic wing theory / by Lomax, Harvard

    Published 1951
    Other Authors: “…Heaslet, M. A. (Maxwell Alfred), 1907-…”
    Government Document Book
  20. 20

    Damping-in-roll calculations for slender swept-back wings and slender wing-body combinations / by Lomax, Harvard

    Published 1949
    Other Authors: “…Heaslet, M. A. (Maxwell Alfred), 1907-…”
    Search for the full-text version of this title in HathiTrust
    Government Document Book
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