The unsteady aerodynamics of a finite supersonic cascade with subsonic axial flow

Journal of Applied Mechanics, Transactions ASME

Volumn 40, Issue 3, 1973, Pages 667-671

  Verdon, J M ^a  

^a UNITED TECHNOLOGIES CORPORATION   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS - SUPERSONIC; MATHEMATICAL MODELS;

FLOW OF FLUIDS;

EID: 0015661362     PISSN: 00218936     EISSN: 15289036     Source Type: Journal    
DOI: 10.1115/1.3423070     Document Type: Article

References (5)

1. Miles, J. W., The Potential Theory of Unsteady Supersonic Flow, Cambridge University Press, 1959.
2. Miles, J. W., “The Compressible Flow Past an Oscillating Airfoil in a Wind Tunnel,” Journal of the Aeronautical Sciences, Vol. 23, July 1956, pp. 671-678.
3. Lane, F., “Supersonic Flow Past an Oscillating Cascade With Supersonic Leading-Edge Locus,” Journal of the Aeronautical Sciences, Vol. 24, Jan. 1957, pp. 65-66.
4. Ashley, H., and Landahl, M., Aerodynamics of Wings and Bodies, Addison-Wesley, Reading, Mass., 1965.
5. Fung, Y. C, An Introduction to the Theory of Aeroelasticity, Wiley, New York, 1955, pp. 166-168.