Effect of Angle of Attack on the Performance of Twin Intake Duct-Reference-Cited by-同舟云学术

Effect of Angle of Attack on the Performance of Twin Intake Duct

Published:2007-06-15 Issue: Volume: Page:
ISSN:
Container-title:37th AIAA Fluid Dynamics Conference and Exhibit
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Author:

Saha Krishnendu¹,Singh Sidh²,Seshadri V.²

Affiliation:

1. Graduate Student, Applied Mechanics Department, Indian Institute of Technology Delhi

2. Professor, Applied Mechanics Department, Indian Institute of Technology Delhi

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2007-4357

Reference20 articles.

1. 1Whitford,R.,DesignforAirCombat,Jane'sPublishing,London,1987.

2. 2Davis, W.F.,and Goldstein, D.L. "Experimental investigationat supersonicspeeds ofTwin-scoop duct inlets ofequal area. I.Aninletenclosing61.5percentofthemaximumcircumference of the forebody", NACA RM-A7J27, Jan.1948.

3. 3Davis, W.F., and Goldstein, D.L. "Experimental investigation at supersonic speeds of twin-scoop duct inlets of equal area. II. Effects of slots upon an inlet enclosed 61.5 percent of the maximum circumference of the forebody", NACA RM-A8C11, June1948.

4. 5Stroud,J.F."ExperimentalInvestigationoftheEffect ofForebodyBluntnessonthe PressureRecoveryand DragofaTwin-Scoop Inlet-BodyCombinationatMachNumbersOf1.4and 1.7,"NACA RM A51K14,Feb.1952.

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