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A Method for Calculating the Aerodynamic Loading on Wing-body Combinations at Small Angles of Attack in Supersonic Flow by Jackson, Charlie M. is a nonfiction available to read on EtoBox.
What is A Method for Calculating the Aerodynamic Loading on Wing-body Combinations at Small Angles of Attack in Supersonic Flow about?
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
Who reads A Method for Calculating the Aerodynamic Loading on Wing-body Combinations at Small Angles of Attack in Supersonic Flow?
It is typically read by self-directed learners exploring a subject in depth.
Common subject areas: history, science, philosophy, social sciences.
- Author
- Jackson, Charlie M.
- Publisher
- National Aeronautics and Space Administration, 1971.
- Published
- 1971
- Language
- EN
- Category
- nonfiction
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