Response of a two-dimensional cascade to an upstream disturbance

AIAA Journal

Volumn 35, Issue 3, 1997, Pages 434-440

  Paynter, Gerald C ^a,b  

^a BOEING COMPANY   (United States)

^b Mail Stop 49 53   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 0000495258     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/3.13523     Document Type: Article

References (5)

1. Hedges, L., Lewis, J., Carlin, C., and Beck, C., "Supersonic Inlet Simulation with Closed Loop Control and Moving Control Surfaces" AIAA Paper 96-0493, Jan. 1996.
2. Cole, G. L., Melcher, K. J., Chicatelli, A. K., Hartley, T. T., and Chung, J. K., "Computational Methods for HSCT-Inlet Controls/CFD Interdisciplinary Research," AIAA Paper 94-3209, June 1994.
3. Steinbrenner, J. P., Chawner, J. R., and Fouts, C. L., "The GRIDGEN 3D Multiple Block Grid Generation System," General Dynamics Corp., WRDC-TR-90-3022, Vols. 1 and 2, Fort Worth, TX, July 1990.
4. Shapiro, A. H., The Dynamics and Thermodynamics of Compressible Fluid Flow, Vol. 2, Ronald, New York, 1954, Chap. 23.
5. Boldman, D. R., lek, C., Hwang, D. P., Larkin, M., and Schweiger, P., "Effect of a Rotating Propeller on the Separation Angle of Attack and Distortion in Ducted Propeller Inlets," AIAA Paper 93-0017, Jan. 1993.