Aerodynamic influence coefficients for an oscillating finite thin wing in supersonic flow
By: Ta Li.
Contributors: Institute of the Aeronautical Sciences (U.S.)
Publisher: Institute of the Aeronautical Sciences
Published: 1956
Place of publication: New York
Number of pages: 46
Notes: Preprint no. 500.

Source: Presented at the 24th Annual Meeting, January 23-26, 1956