Investigation of the longitudinal stability at high speeds of a 1/5-scale model of a tailless pursuit airplane / by Edmund V. Laitone.

Tests of a tailless pursuit airplane model at the Ames Aeronautical Laboratory have shown that in conditions corresponding to level flight at a Mach number less than 0.7 and at an altitude under 35,000 feet, no serious compressibility effects occurred and that no sudden adverse diving moments were e...

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Bibliographic Details
Main Author: Laitone, Edmund V.
Corporate Authors: United States. National Advisory Committee for Aeronautics, Ames Research Center
Other title:NACA Wartime Reports. Series A.
Format: Government Document Book
Language:English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, [1943]
Series:Wartime Reports (United States. National Advisory Committee for Aeronautics) ; no. A77.
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Description
Summary:Tests of a tailless pursuit airplane model at the Ames Aeronautical Laboratory have shown that in conditions corresponding to level flight at a Mach number less than 0.7 and at an altitude under 35,000 feet, no serious compressibility effects occurred and that no sudden adverse diving moments were encountered up to a Mach number of 0.74, the maximum speed of the tests. However, there were indications that the elevons might lose their effectiveness for longitudinal control during a pull-out from a steep dive.
Item Description:NACA Wartime Report A-77.
Originally issued as NACA as a Memorandum Report (March 1943)
Prepared at the Ames Aeronautical Laboratory, Moffett Field, California.
Physical Description:4 pages, 19 unnumbered pages : illustrations ; 27 cm.