Title: Aerodynamic design and analysis system for supersonic aircraft. Part 2: User's manual
Abstract: An integrated system of computer programs for supersonic configurations is described. An explanation of system usage, the input definitions, and example output are included. For Part 1, see N75-18185; for Part 3, see N75-18186.
Publication Year: 1975
Publication Date: 1975-03-01
Language: en
Type: article
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