United States. National Advisory Committee for Aeronautics

Fred E. Weick

Richard W. Noyes

Eastman N. Jacobs

George W. Stickle

K. Hilding Beij

Carl J. Wenzinger

Ira H. Abbott

Ordinary Ailerons on Rectangular Wings. I

Wind-tunnel Research Comparing Lateral Control Devices, Particularly at High Angles of Attack

The Autobiography of an Aeronautical Engineer

From the Ground Up

H. L. Dryden

F. W. Stevens

R. H. Heald

William F. Joachim

A. M. Kuethe

Chester W. Hicks

D. H. Strother

B. H. Monish

Hampton H. Foster

Effect of Variation of Chord and Span of Ailerons on Rolling and Yawing Moments at Several Angles of Pitch

This report, the third of a series of four, describes a simple system for designing propellers of a standard form. In this report, the system is based on tests of a family of model propellers of standard Navy form, the data from which have been extended by means of calculations to cover the complete range likely to be found in practice. However, it can be worked out for any family having propellers of on general form. This system can also be applied as given to propellers of different forms by means of form factors. Modifications are made for full scale flight conditions, i.e., the particular tip speed of the propeller, the body or fuselage interference.

Propeller Design A Simple System Based on Model Propeller Test Data

H. Norman Abramson

These results are intended to provide quantitative flight-test information which may be useful to designers in attempting to provide for adequate low-speed control and which may be correlated with analytical analyses as presented in the third and finai report in this series (Technical Note 3677).

Investigation of Lateral Control Near the Stall Flight Tests with High-wing and Low-wing Monoplanes of Various Configurations

Fred E. Weick

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