In-flight flow visualization results from the X-29A aircraft at high angles of attack / John H. Del Frate and John A. Saltzman.

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Bibliographic Details
Online Access: Online Access
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:

MARC

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264 1 |a [Washington, D.C.] :  |b National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program,  |c November 1992. 
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490 1 |a NASA technical memorandum ;  |v 4430. 
500 |a "November 1992"--Report Documentation page. 
500 |a "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. 
500 |a "Performing organization: NASA Dryden Flight Research Facility"-- Report Documentation page. 
504 |a Includes bibliographical references (pages 13-14) 
513 |a Technical memorandum. 
588 |a Description based on online resource; title from PDF title page (NASA, viewed Feb. 2, 2017) 
536 |a Sponsored by the National Aeronautics and Space Administration  |d WU 533-02-38  |c H-1825. 
650 7 |a Aircraft stability.  |2 nasat. 
650 7 |a Angle of attack.  |2 nasat. 
650 7 |a Flow visualization.  |2 nasat. 
650 7 |a Separated flow.  |2 nasat. 
650 7 |a X-29 aircraft.  |2 nasat. 
700 1 |a Saltzman, John A.,  |e author. 
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