Experimental surface pressure data obtained on 65̊ delta wing across Reynolds number and Mach number ranges [microform] / Julio Chu and James M. Luckring.

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Bibliographic Details
Main Author: Chu, Julio
Corporate Author: Langley Research Center
Other Authors: Luckring, James M.
Other title:Small-radius leading edge.
Format: Government Document Microfilm Book
Language:English
Published: Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], [1996-]
Series:NASA technical memorandum ; 4645.
Subjects:

MARC

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650 0 |a Wind tunnel  |x Examinations. 
650 0 |a Airplanes  |x Wings, Triangular.  |0 http://id.loc.gov/authorities/subjects/sh85002930. 
650 0 |a Reynolds number.  |0 http://id.loc.gov/authorities/subjects/sh85113557. 
650 0 |a Mach number.  |0 http://id.loc.gov/authorities/subjects/sh85079305. 
650 0 |a Aerodynamics.  |0 http://id.loc.gov/authorities/subjects/sh85001295. 
650 7 |a Wind tunnel tests.  |2 nasat. 
650 7 |a Delta wings.  |2 nasat. 
650 7 |a Leading edges.  |2 nasat. 
650 7 |a Reynolds number.  |2 nasat. 
650 7 |a Mach number.  |2 nasat. 
650 7 |a Vortices.  |2 nasat. 
650 7 |a Slender wings.  |2 nasat. 
650 7 |a Pressure distribution.  |2 nasat. 
650 7 |a Subsonic speed.  |2 nasat. 
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740 0 2 |a Small-radius leading edge. 
776 0 8 |i Print version:  |a Chu, Julio.  |t Experimental surface pressure data obtained on 65̊ delta wing across reynolds number and mach number ranges  |w (OCoLC)51039329. 
776 0 8 |i Online version:  |a Chu, Julio.  |t Experimental surface pressure data obtained on 65 ° delta wing across Reynolds number and Mach number ranges  |w (OCoLC)945978511. 
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