Aerodynamic characteristics of a series of twin-inlet air-breathing missile configurations
By: Clyde Hayes
Contributors: United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch
Series: NASA technical memorandum -- 84558-84560
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch; For sale by the National Technical Information Service]
Published: 1983
Place of publication: Washington, D.C; [Springfield, Va
Language: eng
Subjects: Guided missiles -- Control systems; Stability; Aerodynamics
Notes: "March l983"--Cover

Includes bibliographical references
Table of contents: value: 1. Axisymmetric inlets at supersonic speeds; value: 2. Two-dimensional inlets at supersonic speeds; value: 3. Axisymmetric and two-dimensional inlets at subsonic-transonic speeds