Collection and analysis of wind-tunnel data on the characteristics of isolated tail surfaces with and without end plates /

The aerodynamic characteristics of 19 isolated tail surfaces have been determined by wind-tunnel tests and tests have also been made of rectangular airfoils of various aspect ratios with and without double end plates of various shapes. Thes data from these tests have been collected and analyzed

Bibliographic Details
Main Author: Bates, WIlliam R
Corporate Author: United States National Advisory Committee for Aeronautics
Format: Government Document Book
Language:English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, 1947
Series:Technical note (United States. National Advisory Committee for Aeronautics) ; 1291
Subjects:

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Stanford University

Holdings details from Stanford University
Call Number: ISIL:US-CST
NACA TN 1291