Subcritical flows over two dimensional airfoils by a multistrip method of integral relations

  • R. E. Melnik
  • D. C. Ives
Session IV
Part of the Lecture Notes in Physics book series (LNP, volume 8)


Mach Number Integral Relation Airfoil Surface Chebyshev Spacing Strip Boundary 
These keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm improves.


Unable to display preview. Download preview PDF.

Unable to display preview. Download preview PDF.


  1. 1.
    Belotserkovskii, 0. M. and Chushkin, P. I., Basic Developments in Fluid Dynamics 1, 1–123 (ed. M. Holt), Academic Press (1965).Google Scholar
  2. 2.
    Chushkin, P. I., Sb Vych. Mat. 3, 99–110 (1958).Google Scholar
  3. 3.
    Ives, D. C., RM-452, Grumman Aerospace Corporation (1969).Google Scholar
  4. 4.
    Jones, D. J., Private Communication (1970).Google Scholar
  5. 5.
    Knechtel, E. D., NASA TN-D15 (1959).Google Scholar
  6. 6.
    Ludford, G. S. S., J. of Math. and Phy. 30, 131–139 (1951).Google Scholar
  7. 7.
    Sells, C. C. L., Proc. Roy. Soc. A 308, 377–401 (1968).Google Scholar
  8. 8.
    Simisaki, T., Bull. Univ. Osaka Prefecture A 4, 27–35 (1955).Google Scholar
  9. 9.
    Van Dyke, M. D., Private Communication (1970).Google Scholar

Copyright information

© Springer-Verlag 1971

Authors and Affiliations

  • R. E. Melnik
    • 1
  • D. C. Ives
    • 1
  1. 1.Grumman Aerospace CorporationUSA

Personalised recommendations