Non-linear supersonic conical flow over flat plate delta wings
By: John W. Brook.
Contributors: Grumman Aircraft Engineering Corporation. Research Dept
Series: Grumman Aircraft Engineering Corporation. Research Dept. Report -- RE-117
Publisher: Grumman Aircraft Engineering Corporation, Research Dept
Published: 1959
Place of publication: Long Island, N.Y
Number of pages: 110
Notes: Bibliographical references: p.80-81.