Experimental Surface Pressure Data Obtained on 65 Deg Delta Wing Across Reynolds Number and Mach Number Ranges

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Total Pages	: 34
Release	: 1996
ISBN-10	: NASA:31769000523608
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Rating	: 4/5 ( Downloads)

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Book Synopsis Experimental Surface Pressure Data Obtained on 65 Deg Delta Wing Across Reynolds Number and Mach Number Ranges by :

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An experimental wind tunnel test of a 65 deg delta wing model with interchangeable leading edges was conducted in the Langley National Transonic Facility (NTF).