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Can I read Boundary-layer transition study of several pointed bodies of revolution at supersonic speeds, by William A. Cassels and James F. Campbell. on EtoBox?
Boundary-layer transition study of several pointed bodies of revolution at supersonic speeds, by William A. Cassels and James F. Campbell. by Cassels, William A. is a nonfiction available to read on EtoBox.
What is Boundary-layer transition study of several pointed bodies of revolution at supersonic speeds, by William A. Cassels and James F. Campbell. about?
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
Who reads Boundary-layer transition study of several pointed bodies of revolution at supersonic speeds, by William A. Cassels and James F. Campbell.?
It is typically read by self-directed learners exploring a subject in depth.
Common subject areas: history, science, philosophy, social sciences.
- Author
- Cassels, William A.
- Publisher
- National Aeronautics and Space Administration; [for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va.] 1970.
- Published
- 1970
- Language
- EN
- Category
- nonfiction