Determination of the Stability and Control Characteristics of Airplanes from Tests of Powered Models
Release on 1942 | by Isidore G. Recant

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
  • Author: Isidore G. Recant
  • Publisher:
  • ISBN: UOM:39015095014935
  • Category: Airplanes
  • Page: 41
  • View: 927

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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