one-parameter method for the calculation of laminar compressible boundary-layer flow with a pressure gradient
By: J. A. Zaat.
Contributors: National Aeronautical Research Institute (Netherlands)
Series: National Aeronautical Research Institute. Report -- F. 141
Publisher: National Aeronautical Research Institute
Published: 1953
Place of publication: Amsterdam
Number of pages: 32
Notes: Bibliographical references: p. 29.