Quarterly of Applied Mathematics

Quarterly of Applied Mathematics

Online ISSN 1552-4485; Print ISSN 0033-569X



The aerodynamics of supersonic biplanes

Authors: W. R. Sears and H. S. Tan
Journal: Quart. Appl. Math. 9 (1951), 67-76
MSC: Primary 76.1X
DOI: https://doi.org/10.1090/qam/44988
MathSciNet review: 44988
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References [Enhancements On Off] (What's this?)

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  • [3] Max A. Heaslet and Harvard Lomax, The use of source-sink and doublet distributions extended to the solution of arbitrary boundary value problems in supersonic flow, Tech. Notes. Nat. Adv. Comm. Aeronaut., 1948 (1948), no. 1515, 48. MR 0023159
  • [4] John C. Evvard, Distribution of wave drag and lift in the vicinity of wing tips at supersonic speeds, Tech. Notes Nat. Adv. Comm. Aeronaut., 1947 (1947), no. 1382, 28 pp. (5 plates). MR 0020900
  • [5] John C. Evvard and L. Richard Turner, Theoretical lift distribution and upwash velocities for thin wings at supersonic speeds, Tech. Notes Nat. Adv. Comm. Aeronaut., 1947 (1947), no. 1484, 36 pp. (12 plates). MR 0022130
  • [6] Maxime Bocher, An introduction to the study of integral equations, Cambridge University Press, 1909.
  • [7] M. J. Lighthill, The supersonic theory of wings of finite span, Rep. and Memoranda no. 2001 (8079), Ministry of Supply [London], Aeronaut. Res. Council, 1944. MR 0017091
  • [8] H. S. Tan, The wave drag of a supersonic biplane of finite span, A thesis submitted in partial fulfillment of the requirements for the degree Ph.D., Cornell University, 1949.

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DOI: https://doi.org/10.1090/qam/44988
Article copyright: © Copyright 1951 American Mathematical Society

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