Applications of Busemann inlet designs for flight at hypersonic speeds
Author:
Affiliation:
1. Johns Hopkins University, Laurel, MD
2. Ryerson Polytechnical Institute, Toronto, Canada
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1992-1210
Reference17 articles.
1. Delta Wings of Shapes Amenable to Exact Shock-wave Theory
2. Maikapar, G.I. "Bodies Formed by the Stream Surfaces of Conical Flows,"Fluid Dynamics,Vol. 1, No. 1, 1966.
3. A class of three-dimensional, optimum hypersonic wings.
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