Ahmed, Sajeer (1998) Experimental investigation on cone cylinder bodies of elliptical and circular cross sections at M = 2.0 AIAA Paper 98-2727. In: 16th AIAA Applied Aerodynamics Conference, June 15-18, 1998, Albuquerque, NM.
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Abstract
This paper deals with an experimental investigation of a family of cone-cylinder bodies having circular and equivalent elliptical (a/b = 2.0) cross sections with variation in nose and afterbody fineness ratios at Mach number 2.0. All elliptical bodies are tested at roll orientations of 0 deg (semimajor axis normal to cross flow velocity) and 90 deg (semiminor axis normal to crossflow velocity). The nose fineness ratios for these bodies are 1.0, 2.0, and 3.0, and the afterbody fineness ratios are 5.0 and 7.0. The effect of changing the cross section shape from circular to elliptical, the roll orientation, and the variation in nose and afterbody fineness ratios on aerodynamic characteristics are discussed. (Author)
| Item Type: | Conference or Workshop Item (Paper) |
|---|---|
| Uncontrolled Keywords: | Circular cylinders;Mach cones;Elliptical cylinders; Afterbodies;Lift drag ratio |
| Subjects: | AERONAUTICS > Aeronautics (General) |
| Depositing User: | Mr. N A |
| Date Deposited: | 22 Aug 2008 |
| Last Modified: | 24 May 2010 04:10 |
| URI: | http://nal-ir.nal.res.in/id/eprint/1033 |
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