Turbulent Boundary Layer Studies on a Waisted Body of Revolution in Subsonic and Supersonic Flow
Title | Turbulent Boundary Layer Studies on a Waisted Body of Revolution in Subsonic and Supersonic Flow PDF eBook |
Author | Kenneth George Winter |
Publisher | |
Pages | 13 |
Release | 1965 |
Genre | Aerodynamics |
ISBN |
Studies of the Turbulent Boundary Layer on a Waisted Body of Revolution in Subsonic and Supersonic Flow
Title | Studies of the Turbulent Boundary Layer on a Waisted Body of Revolution in Subsonic and Supersonic Flow PDF eBook |
Author | K. G. Winter |
Publisher | |
Pages | 76 |
Release | 1968 |
Genre | |
ISBN |
Studies of the Turbulent Boundary Layer on a Waisted Body of Revolution in Subsonic and Supersonic Flow
Title | Studies of the Turbulent Boundary Layer on a Waisted Body of Revolution in Subsonic and Supersonic Flow PDF eBook |
Author | K. G. Winter |
Publisher | |
Pages | 76 |
Release | 1968 |
Genre | |
ISBN | 9780114703332 |
Studies of the Turbulent Boundary Layer on a Waisted Body of Revolution in Subsonic and Supersonic Flow
Title | Studies of the Turbulent Boundary Layer on a Waisted Body of Revolution in Subsonic and Supersonic Flow PDF eBook |
Author | Kenneth George Winter |
Publisher | |
Pages | 75 |
Release | 1970 |
Genre | Aerodynamics |
ISBN |
Studies of the Turbulent Boundary Layer on a Waised Body of Revolution in Subsonic and Supersonic Flow
Title | Studies of the Turbulent Boundary Layer on a Waised Body of Revolution in Subsonic and Supersonic Flow PDF eBook |
Author | Aeronautical Research Council |
Publisher | |
Pages | |
Release | 1970 |
Genre | |
ISBN |
Boundary-layer Transition Study of Several Pointed Bodies of Revolution at Supersonic Speeds
Title | Boundary-layer Transition Study of Several Pointed Bodies of Revolution at Supersonic Speeds PDF eBook |
Author | William A. Cassels |
Publisher | |
Pages | 76 |
Release | 1970 |
Genre | Aerodynamics, Supersonic |
ISBN |
Boundary-layer transition by the sublimation and impact-pressure techniques and force tests have been performed on three Haack-Adams bodies of revolution of fineness ratios 7, 10, and 13 at zero angle of attack for free-stream Mach numbers of 2.00, 2.75, and 4.63 and a range of Reynolds numbers based on model length of 6 to 15 X 10(to the 6 power) with and without a roughness strip. The grit method of inducing turbulence was found to provide for a nearly complete turbulent flow over the models at the lower Mach numbers and higher Reynolds numbers considered in this study while the amount of trip drag was less than 8 percent of the model drag with transition fixed. A method of interpreting sublimation data was discussed and used and the results compared well with the impact-pressure results.
Reports and Memoranda - Aeronautical Research Council
Title | Reports and Memoranda - Aeronautical Research Council PDF eBook |
Author | Aeronautical Research Council (Great Britain) |
Publisher | |
Pages | 88 |
Release | 1970 |
Genre | Aeronautics |
ISBN |
Beginning with no. 650 each hundredth number contains a list of the Reports and memoranda published since the last list.