Compressibility Effects in Unsteady Thin-Airfoil Theory
Author:
Affiliation:
1. United Aircraft Research Laboratories, East Hartford, Conn.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference9 articles.
1. Unsteady thin-airfoil theory for subsonic flow.
2. On the Compressibility Correction for Subsonic Unsteady Flow
3. A note on Riemann’s method applied to the diffusion equation
4. Similarity rules for thin aerofoils in non-stationary subsonic flows
5. Adamczyk, J. J. "Passage of an Isolated Airfoil Through a Three-Dimensional Disturbance," Ph.D. thesis,1971, Univ. of Connecticut, Storrs, Conn.; also Rept. UAR-K97, 1971, United Aircraft Corp, East Hartford, Conn.
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