Boundary Layer Transition Study Of Several Pointed Bodies Of Revolution At Supersonic Speeds
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Boundary-layer Transition Study of Several Pointed Bodies of Revolution at Supersonic Speeds
Author | : William A. Cassels |
Publisher | : |
Total Pages | : 76 |
Release | : 1970 |
Genre | : Aerodynamics, Supersonic |
ISBN | : |
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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.
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