Pilot-pressure Measurements in Flow Fields Behind a Rectangular Nozzle with Exhaust Jet for Free-stream Mach Numbers of 0.00, 0.60, and 1.20

Pilot-pressure Measurements in Flow Fields Behind a Rectangular Nozzle with Exhaust Jet for Free-stream Mach Numbers of 0.00, 0.60, and 1.20
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Publisher :
Total Pages : 160
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ISBN-10 : NASA:31769000575673
ISBN-13 :
Rating : 4/5 (73 Downloads)

Book Synopsis Pilot-pressure Measurements in Flow Fields Behind a Rectangular Nozzle with Exhaust Jet for Free-stream Mach Numbers of 0.00, 0.60, and 1.20 by :

Download or read book Pilot-pressure Measurements in Flow Fields Behind a Rectangular Nozzle with Exhaust Jet for Free-stream Mach Numbers of 0.00, 0.60, and 1.20 written by and published by . This book was released on 1986 with total page 160 pages. Available in PDF, EPUB and Kindle. Book excerpt:


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Language: en
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Measured and Theoretical Flow Fields Behind a Rectangular and a Triangular Wing Up to High Angles of Attack at a Mach Number of 2.46
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Effect of Mach Number on Position Error as Applied to a Pitot-static Tube Located 0.55 Chord Ahead of an Airplane Wing
Language: en
Pages: 20
Authors: W. F. Lindsey
Categories: Aerodynamics
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Summary: The effect on static-pressure measurements of locating a pitot-static tube 0.55 chord ahead of an airfoil section has been investigated. The tests were