Influence of the leading-edge shock wave on the laminar boundary layer at hypersonic speeds
By: sponsored by United States Army Ordnance and United States Air Force.
Contributors: Daniel Guggenheim Aeronautical Laboratory
Publisher: California Institute of Technology, Guggenheim Aeronautical Laboratory
Published: 1954
Place of publication: Pasadena, Calif
Number of pages: 26
Notes: Technical report no. 1.

Contract number: DA-04-495-Ord-19