The Extension of Analytic Hypersonic Force Coefficients for Conceptual Design Using the Divergence Theorem

Author:

Grant Michael1,Braun Robert1

Affiliation:

1. Georgia Institute of Technology

Publisher

American Institute of Aeronautics and Astronautics

Reference29 articles.

1. Aero-Thermodynamics for Conceptual Design

2. 4Bonner,E.,Clever,W.,andDunn,K.“AerodynamicPreliminaryAnalysisSystemII:PartITheory,”NASA-CR-165627, Apr. 1981.

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