Design and predictions for a high-altitude (low-Reynolds-number) aerodynamic flight experiment / Donald Greer [and three others]

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Bibliographic Details
Online Access: Online Access
Main Author: Greer, Donald, 1896- (Author)
Format: Government Document eBook
Language:English
Published: Edwards, California : National Aeronautics and Space Administration, Dryden Flight Research Facility, July 1999.
Series:NASA technical memorandum ; 1999-206579.
Subjects:

MARC

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245 1 0 |a Design and predictions for a high-altitude (low-Reynolds-number) aerodynamic flight experiment /  |c Donald Greer [and three others] 
264 1 |a Edwards, California :  |b National Aeronautics and Space Administration, Dryden Flight Research Facility,  |c July 1999. 
300 |a 1 online resource (17 pages) :  |b illustrations. 
336 |a text  |b txt  |2 rdacontent. 
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490 1 |a NASA/TM ;  |v 1999-206579. 
500 |a "July 1999." 
500 |a "Presented at the 17th Applied Aerodynamics Conference and 14th Computational Fluid Dynamics Conference, Norfolk, Virginia, June 28-July 1, 1999, AIAA 99-3183"--Report documentation page. 
500 |a "Performing organization: NASA Dryden Flight Research Center and Technische Universität München"--Report documentation page. 
504 |a Includes bibliographical references (pages 16-17) 
513 |a Technical memorandum. 
588 |a Description based on online resource; title from PDF title page (NASA, viewed Aug. 18, 2017) 
536 |a Sponsored by the National Aeronautics and Space Administration  |d 529-1004-0029-00-APE  |d H-2340. 
650 7 |a Airfoils.  |2 nasat. 
650 7 |a High altitude.  |2 nasat. 
650 7 |a Low Reynolds number.  |2 nasat. 
650 7 |a Navier-Stokes equation.  |2 nasat. 
650 7 |a Aerodynamic drag.  |2 nasat. 
650 7 |a Static pressure.  |2 nasat. 
650 7 |a Subsonic speed.  |2 nasat. 
650 7 |a Boundary layer stability.  |2 nasat. 
650 7 |a Flight tests.  |2 nasat. 
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