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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Main Author: | |
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Corporate Authors: | , |
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. |
Subjects: |
Search Result 1
The high-speed characteristics of several flaps and spoilers on the upper surface of the horizontal stabilizer of a model of a radial-engine pursuit airplane /
Published 1946
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High-speed wind-tunnel tests of a twin-fuselage pursuit airplane /
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Tests of a jet-motor air-intake duct system on a 1/4-scale stub-wing model of a pursuit-type airplane /
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An additional investigation of the high-speed lateral-control characteristics of spoilers /
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Aerodynamic characteristics of a 1/8-scale powered model of a high-speed bomber with a dual pusher propeller aft of the empennage /
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A comparison of analytically and experimentally determined isothermal pressure losses in a heat-exchanger installation /
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A comparison of two flight-test procedures for the determination of aileron control capabilities of an airplane /
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Computation of hinge-moment characteristics of horizontal tails from section data /
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Correlation of the drag characteristics of a P-51B airplane obtained from high-speed wind-tunnel and flight tests /
Published 1945
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Correlation of wind-tunnel predictions with flight tests of a twin-engine patrol airplane. : 1 - Longitudinal-stability and -control characterstics /
Published 1945
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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 /
Published 1945
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Effect of the performance of a turbosupercharged engine of an exhaust-gas-to-air heat exchanger for thermal ice prevention /
Published 1945
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The effect of the skis on the power-off stability characteristics of a twin-engine cargo airplane /
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The effect of wall interference upon the aerodynamic characteristics of an airfoil spanning a closed-throat circular wind tunnel /
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An experimental investigation of the effect of propellers used as aerodynamic brakes on stability and control /
Published 1945
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Search Result 20
A flight investigation of the ice-prevention requirements of the United States Naval K-Type airship /
Published 1945
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