Pressure distributions on three different cruciform aft-tail control surfaces of a wingless missile at mach 1.60, 2.36, and 3.70
By: Milton Lamb ... [et al.]
Contributors: Lamb, Milton; United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch
Series: NASA technical memorandum -- 80097
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch; For sale by the National Technical Information Service]
Published: 1979
Place of publication: Washington, D.C; [Springfield, Va
Language: eng
Subjects: Aerodynamics
Notes: "August 1979"--Cover

Subject category 02
Table of contents: value: v. 1. Trapezoidal tail; value: v. 2. Clipped delta tail; value: v. 3. Cranked tail