The effect of Mach number on the aerodynamic characteristics of a single-engine pursuit airplane as determined from tests of a 1/3-scale model /

The effect of Mach number on the aerodynamic characteristics of a single-engine pursuit airplane as determined from tests of a 1/3-scale model / by Robert C. Robinson and Henry Jessen.

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Presented herein are the results of tests to determine the effects of Mach number on the aerodynamic characteristics of an Allison powered single-engine pursuit airplane. The lift, drag, and pitching-moment characteristics at high speed are discussed and data are included to show the variation of st...

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Bibliographic Details
Main Author: Robinson, Robert C.
Corporate Authors: United States. National Advisory Committee for Aeronautics, Ames Research Center
Other Authors: Jessen, Henry
Other title:NACA Wartime Reports. Series A.
Format: Government Document Book
Language:English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, [1945]
Series:Wartime Reports (United States. National Advisory Committee for Aeronautics) ; no. A76.
Subjects:
Fighter planes.
Airplanes > Models.
Lift (Aerodynamics)
Drag (Aerodynamics)
Pitching (Aerodynamics)
Stability of airplanes.
Airplanes > Control.
Mach number.
Wind tunnel testing.

Norlin Library - Basement - Government Information - US

Holdings details from Norlin Library - Basement - Government Information - US
Call Number: Y 3.N 21/5:11/A76
Y 3.N 21/5:11/A76 Available Place a Hold

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