A Method for Determining the Total Drag of a Pointed Body of Revolution in Supersonic Flow with Turbulent Boundary Layer
Author | : Charlie M. Jackson |
Publisher | : |
Total Pages | : 74 |
Release | : 1969 |
Genre | : Boundary layer |
ISBN | : |
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Author | : Charlie M. Jackson |
Publisher | : |
Total Pages | : 74 |
Release | : 1969 |
Genre | : Boundary layer |
ISBN | : |
Author | : Charlie M. Jackson |
Publisher | : |
Total Pages | : 44 |
Release | : 1971 |
Genre | : Aerodynamics, Supersonic |
ISBN | : |
This report describes a theoretical method for estimating the aerodynamic loading on a wing-body configuration. In order to provide a basis for evaluation of the method, experimental measurements of surface pressures, forces, and moments were made on a series of basic wing-body configurations over a Mach number range from 2.5 to 4.5. Comparison of the theoretical estimates with these experimental data generally indicated good agreement for the entire range of configurations and test conditions.
Author | : United States. Superintendent of Documents |
Publisher | : |
Total Pages | : 1348 |
Release | : 1970 |
Genre | : United States |
ISBN | : |
Author | : United States. Superintendent of Documents |
Publisher | : |
Total Pages | : 1464 |
Release | : 1966 |
Genre | : Government publications |
ISBN | : |
Author | : United States. National Aeronautics and Space Administration Scientific and Technical Information Division |
Publisher | : |
Total Pages | : 966 |
Release | : 1970 |
Genre | : Aeronautics |
ISBN | : |
Author | : United States. National Aeronautics and Space Administration. Scientific and Technical Information Division |
Publisher | : |
Total Pages | : 962 |
Release | : 1970 |
Genre | : Aeronautics |
ISBN | : |
Author | : United States. National Aeronautics and Space Administration. Scientific and Technical Information Division |
Publisher | : |
Total Pages | : 956 |
Release | : 1970 |
Genre | : Science |
ISBN | : |