Determination of the Stability and Control Characteristics of Airplanes from Tests of Powered Models

The Influence of Running Propellers 02 Airplane Characteristics . Jour of Aero . Sci . , vol . 17 , no . 3 , Jar . 1940 , pp . 85-106 , 3 . Donlan , C. J. , and Recant , I. G .: Methods of Analyzine Vind - Tunnel Data for Dynamic Flight ...

Determination of the Stability and Control Characteristics of Airplanes from Tests of Powered Models

A technique of testing wind-tunnel powered models has been developed as a result of experience gained in the investigation of the static longitudinal and lateral stability and control characteristics of several powered models in the NACA 7- by 10-foot wind tunnel. As an important part of this technique, a minimum program of the tests considered necessary to specify satisfactorily the static stability and control characteristics for present-day airplanes has been tentatively established.

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Aircraft characteristics. pt. 1. Civil aircraft by Cornell Aeronautical Laboratory
Language: en
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Authors: Mineola (N.Y.). Airborne Instruments Laboratory
Categories: Aeronautics
Type: BOOK - Published: 1957 - Publisher:

Books about Aircraft characteristics. pt. 1. Civil aircraft by Cornell Aeronautical Laboratory
Airplane Characteristics
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Pages: 123
Authors: Frederick Bedell
Categories: Airplanes
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NACA Conference on Some Problems of Aircraft Operation
Language: en
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Authors: United States. National Advisory Committee for Aeronautics
Categories: Aeronautics
Type: BOOK - Published: 1955 - Publisher:

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NASA Memorandum
Language: en
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Authors: United States. National Advisory Committee for Aeronautics
Categories: Aeronautics
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Books about NASA Memorandum
High Speed Problems of Aircraft and Experimental Methods
Language: en
Pages: 1024
Authors: Allen F. Donovan
Categories: Science
Type: BOOK - Published: 2015-12-08 - Publisher: Princeton University Press

Volume VIII of the High Speed Aerodynamics and Jet Propulsion series. This volume includes: performance calculation at high speed; stability and control of high speed aircraft; aeroelasticity and flutter; model testing; transonic wind tunnels; supersonic tunnels; hypersonic experimental facilities; low density wind tunnels; shock tube; wind tunnel measurements; instrumented models