Summary
In this paper a review of the recent developments in the theory of a slowly oscillating low aspect ratio, pointed wing at sonic speed is presented, using the concepts of the parabolic method, the equivalence rule and a iteration method to approximately incorporate the thickness effect in the analysis.
This is a preview of subscription content, log in via an institution to check access.
Access this chapter
Tax calculation will be finalised at checkout
Purchases are for personal use only
Preview
Unable to display preview. Download preview PDF.
References
Oswatitsch, K., Keune, E: The flow around bodies of revolution at Mach number 1. Proceedings of the conference on high-speed aeronautics, pp. 113–131. Polytechnic Institute of Brooklyn, New York (1955).
Hosokawa, I.: A simplified analysis for transonic flows around thin bodies. In: Symposium Transsonicum (Oswatitsch, K. ed.), pp. 184 —199. IUTAM Symposium, Aachen, Germany 1962. Berlin Göttingen Heidelberg: Springer 1964.
Teipel, I.: Die instationären Luftkräfte bei der Machzahl 1. Z. Flugwiss. 12, 6–14 (1964).
Ruo, S. Y., Liu, D. D.: Calculation of stability derivatives for slowly oscillating bodies of revolution at Mach 1. Lockheed Missiles and Space Co. LMSC/HREC D162375 (1971).
Zierep, J.: Der Äquivalenzsatz and die parabolische Methode für schallnahe Strömungen. ZAMM 45, 19–27 (1965).
Adams, M. C., Sears, W. R.: Slender-body theory — review and extension. J. Aero. Sci. 20, 85 — 98 (1953).
Landahl, M. T.: Unsteady transonic flow. New York: Pergamon Press 1961.
Kimble, K. R., Liu, D. D., Ruo, S. Y., Wu, J. M.: Unsteady transonic flow analysis for low aspect ratio, pointed wings. AIAA J. 12, 516–522 (1974).
Ruo, S. Y.: Slowly oscillating pointed low aspect ratio wings at sonic speed with thickness effect. ZAMM 54, 119 —121 (1974).
Sapunkova, O. M.: Slowly oscillating pointed low aspect ratio wings at sonic speed. Aerodynamica (Transonic Flow), University of Saratov, 52–60 (1981).
Liu, D. D., Platzer, M. F., Ruo, S. Y.: Unsteady linearized transonic flow analysis for slender bodies. AIAA J. 15, 966 — 973 (1977).
Oswatitsch, K.: Similarity and equivalence in compressible flow. Advances in applied mechanics, Vol. VI, pp. 153–271. New York: Academic Press 1960.
Author information
Authors and Affiliations
Editor information
Editors and Affiliations
Rights and permissions
Copyright information
© 1994 Springer-Verlag
About this chapter
Cite this chapter
Turbatu, S. (1994). The boundary value problem for low aspect ratio, pointed wings at sonic speed Recent developments in theory. In: Schnerr, G.H., Bohning, R., Frank, W., Bühler, K. (eds) Fluid- and Gasdynamics. Acta Mechanica, vol 4. Springer, Vienna. https://doi.org/10.1007/978-3-7091-9310-5_18
Download citation
DOI: https://doi.org/10.1007/978-3-7091-9310-5_18
Publisher Name: Springer, Vienna
Print ISBN: 978-3-211-82495-5
Online ISBN: 978-3-7091-9310-5
eBook Packages: Springer Book Archive