A flight investigation of internally balanced sealed ailerons in the presence of a balanced split flap /

A flight investigation of internally balanced sealed ailerons in the presence of a balanced split flap / by W.C. Williams.

Show other versions (792)

Flight tests were made with a modified Eyan ST airplane to determine the effect of aileron characteristics of various arrangements of balanced split flaps covering that portion of the wing span occupied by the ailerons. NACA recording instruments were used to determine the aileron effectiveness.

Saved in:
Bibliographic Details
Main Author: Williams, W. C.
Corporate Authors: United States. National Advisory Committee for Aeronautics, Langley Aeronautical Laboratory
Other title:NACA Wartime Reports. Series L.
Format: Government Document Book
Language:English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, [1942]
Series:Wartime Reports (United States. National Advisory Committee for Aeronautics) ; no. L242.
Subjects:
Airplanes > Wings.
Flaps (Airplanes)
Ailerons.
Split flaps (Airplanes)
Airplanes > Flight testing.
Charts, diagrams, etc.

Norlin Library - Basement - Government Information - US

Holdings details from Norlin Library - Basement - Government Information - US
Call Number: Y 3.N 21/5:11/L242
Y 3.N 21/5:11/L242 Available Place a Hold

Similar Items