Wind-tunnel investigation of control-surface characteristics. : 26 - Pressure distribution over an NACA 0009 airfoil with 0.30-airfoil-chord beveled-trailing-edge flaps / by H. Page Hoggard, Jr. and Marjorie E. Bulloch.

Saved in:

Bibliographic Details
Main Author:	Hoggard, H. Page
Corporate Authors:	United States. National Advisory Committee for Aeronautics, Langley Aeronautical Laboratory
Other Authors:	Bulloch, Marjorie E.
Other title:	NACA Wartime Reports. Series L.
Format:	Government Document Book
Language:	English
Published:	Washington, D.C. : National Advisory Committee for Aeronautics, [1944]
Series:	Wartime Reports (United States. National Advisory Committee for Aeronautics) ; no. L205.
Subjects:	Aerofoils. Airplanes > Control surfaces. Flaps (Airplanes) Trailing edges (Aerodynamics) Aerodynamic load. Hinge moments (Aerodynamics) Wind tunnel 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/L205
Y 3.N 21/5:11/L205	Available Place a Hold