Numerical investigations on the solution of the non-linear equation of supersonic flow by finite difference methods (Part 1)
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: 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: 45
Notes: Technical note, no. 10.

Bibliographical references: p. 41-42.

Contract number: AF-61(514)-1080