Linear supersonic flow past combinations of a cylindrical body and triangular wings
By: research sponsored in part by the Office of Scientific Research of the Air Research and Development Command, United States Air Force, through its European office.
Contributors: Stetter, Hans J.; Technische Hochschule Munchen. Mathematical Institute; U.S. Air Force. Office of Scientific Research
Publisher: U.S. Air Force, Office of Scientific Research, Air Research and Development Command
Published: 1959
Place of publication: [S.l.]
Number of pages: 28
Notes: Technical note, no. 11.

Contract number: AF-61(514)-1080