Effects of wing incidence on the longitudinal trim characteristics of a cambered 70° delta-wing configuration at mach numbers 3.0 to 5.0 /
by Warren F. Ahtye.

Description

Main Author: Ahtye, Warren F.
Related Names: Ames Research Center.
Language(s): English
Published: Washington, D.C. : National Aeronautics and Space Administration, 1960.
Subjects: Fighter planes > Fighter planes / Safety measures > Fighter planes / Safety measures / Testing.
Stability of airplanes, Longitudinal > Stability of airplanes, Longitudinal / Testing.
Airplanes > Airplanes / Wings, Triangular > Airplanes / Wings, Triangular / Testing.
Delta wing airplanes > Delta wing airplanes / Stability > Delta wing airplanes / Stability / Testing.
Note: "September 1960."
Cover title.
Full text also available online. Address as of 11/15/2010:
Physical Description: 52 p. : ill. ; 26 cm.
Locate a Print Version: Find in a library

Item Link	Original Source
Full view	University of Illinois at Urbana-Champaign