Experimental aerodynamic characteristics for bodies of elliptic cross section at angles of attack from 0 ̊to 58 ̊and Mach numbers from 0.6 to 2.0 /
Leland H. Jorgensen and Edgar R. Nelson.
Description
- Language(s)
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English
- Published
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Washington, D.C. : National Aeronautics and Space Administration ; 1975.
- Summary
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An experimental investigation was conducted in the Ames 6- by 6-Foot Wind Tunnel to measure the static aerodynamic characteristics for two bodies of elliptic cross section and for their equivalent body of revolution. The equivalent body of revolution had the same length and axial distribution of cross-sectional area as the elliptic bodies. It consisted of a tangent ogive nose of fineness ratio 3 followed by a cylinder with a fineness ratio of 7. For the first body of elliptic cross section, the ratio of the semimajor axis to semiminor axis was held constant at 2 all along the body length. For the second elliptic body the nose was unchanged, but the aftersection was changed as follows: The cross-sectional axis ratio a/b was decreased from 2 to 1 over an axial distance of about 1.66 diam. Then, at this position, the a,b axis system was rotated 90⁰, and the a/b ratio was increased back to 2 over the next 2.34 diam in length. Over the last length of three body diam, this rotated a/b ratio was held constant at 2.
- Note
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Prepared at Ames Research Center.
Cover title.
- Physical Description
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iv, 77 p. :
chiefly ill. ;
27 cm.
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University of Illinois at Urbana-Champaign
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