Cover Image

In-flight flow visualization results from the X-29A aircraft at high angles of attack /

Bibliographic Details
Main Authors: Del Frate, John H. (Author), Saltzman, John A. (Author)
Corporate Author: Dryden Flight Research Facility
Format: Government Document eBook
Language:English
Published: [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, November 1992.
Series:NASA technical memorandum ; 4430.
Subjects:
Aircraft stability.
Angle of attack.
Flow visualization.
Separated flow.
X-29 aircraft.
Online Access:https://purl.fdlp.gov/GPO/gpo77088
Description
Item Description:"November 1992"--Report Documentation page.
"This paper was prepared as AIAA paper 92-4102 for the 6th Biennial Right Test Conference at Hilton Head, South, Carolina, August 24-26, 1992"--Report documentation page.
"Performing organization: NASA Dryden Flight Research Facility"-- Report Documentation page.
Physical Description:1 online resource (14 pages) : illustrations.
Bibliography:Includes bibliographical references (pages 13-14).