An edition of Pressure distributions on three different cruciform aft-tail control surfaces of a wingless missile at mach 1.60, 2.36, and 3.70

Pressure distributions on three different cruciform aft-tail control surfaces of a wingless missile at mach 1.60, 2.36, and 3.70
Pressure distributions on three different cru ...
Milton Lamb ... [et al.]
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Last edited by MARC Bot
January 23, 2026 | History
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An edition of Pressure distributions on three different cruciform aft-tail control surfaces of a wingless missile at mach 1.60, 2.36, and 3.70

Pressure distributions on three different cruciform aft-tail control surfaces of a wingless missile at mach 1.60, 2.36, and 3.70

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Publish Date
Publisher
National Aeronautics and Space Administration, Scientific and Technical Information Branch, For sale by the National Technical Information Service]
Language
English

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Subjects

Aerodynamics
Edition Availability
Cover of: Pressure distributions on three different cruciform aft-tail control surfaces of a wingless missile at mach 1.60, 2.36, and 3.70
Pressure distributions on three different cruciform aft-tail control surfaces of a wingless missile at mach 1.60, 2.36, and 3.70
1979, National Aeronautics and Space Administration, Scientific and Technical Information Branch, For sale by the National Technical Information Service]
in English

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Book Details

Table of Contents

v. 1. Trapezoidal tail
v. 2. Clipped delta tail
v. 3. Cranked tail

Edition Notes

"August 1979"--Cover

Subject category 02

Published in
Washington, D.C, [Springfield, Va
Series
NASA technical memorandum -- 80097

The Physical Object

Pagination
3 v. :

Edition Identifiers

Open Library
OL14925609M

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