The subsonic static aerodynamic characteristics of an airplane model having a triangular wing of aspect ratio 3

The subsonic static aerodynamic characteristics of an airplane model having a triangular wing of aspect ratio 3 2, Lateral and directional characteristics /

An investigation has been conducted to determine the effects of vertical-tail location and size on the subsonic aerodynamic characteristics of a model having a triangular wing. The wing had an aspect ratio of 3, an NACA 0003.5-63 section in the streamwise direction, and plain, trailing-edge ailerons...

Full description

Saved in:
Bibliographic Details
Main Author: Savage, Howard F
Corporate Author: United States National Advisory Committee for Aeronautics
Other Authors: Tinling, Bruce E
Format: Government Document Book
Language:English
Published: Washington : National Advisory Committee for Aeronautics, [1957]
Series:Technical note (United States. National Advisory Committee for Aeronautics) ; 4042
Subjects:
Aerodynamics
Airplanes > Models > Testing
Airplanes > Wings, Triangular
Stability of airplanes, Lateral
Wind tunnel testing
Tags: Add Tag
No Tags, Be the first to tag this record!

Internet

This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.

Stanford University

Holdings details from Stanford University
Call Number: ISIL:US-CST
NACA TN 4042

Similar Items