Description: Numerical solution of the hypersonic viscous-shock-layer equations for laminar, transitional and turbulent flows of a perfect gas over blunt axially symmetric bodies/

Main Author:	Anderson, E. Clay
Corporate Authors:	United States National Aeronautics and Space Administration, United States. National Aeronautics and Space Administration, Langley Research Center
Other Authors:	Moss, James N.
Format:	Book
Language:	English
Published:	Washington: U.S. National Aeronautics and Space Administration, 1975
Series:	NASA technical note 7865
Subjects:	Aerodynamics, Hypersonic > Mathematical models Viscous flow > Mathematical models Shock waves > Mathematical models Laminar flow > Mathematical models Transition flow > Mathematical models Turbulence > Mathematical models

Physical Description:	35 σ. : εικ. ; 27 εκ.
Bibliography:	Βιβλιογραφία: σ. 28-29