Wind-tunnel investigations of blunt-body drag reduction using forebody surface roughness

Author:

Whitmore Stephen1,Sprague Stephanie2,Naughton Jonathan3

Affiliation:

1. NASA, Dryden Flight Research Center, Edwards, CA

2. Kansas, Univ., Lawrence

3. Wyoming, Univ., Laramie

Publisher

American Institute of Aeronautics and Astronautics

Reference29 articles.

1. Test Procedures

2. 4211+0.7611-0.4=

Cited by 9 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Effects of Low Subsonic Wind Tunnel Model Hardware Surface Treatments on Drag;53rd AIAA Aerospace Sciences Meeting;2015-01-02

2. Sounding Rocket Energy Management Using Cold-Gas Aerospike Thrusters;47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2011-07-31

3. Base Drag Reduction of 2D Bluff Body by Using Tabs at Transonic Speeds;JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2008

4. Experimental Investigation of the Wake Structure Responsible for Reduced Base Drag;3rd AIAA Flow Control Conference;2006-06-05

5. A Comparison of Bluff-Body Base-Drag Reduction by Passive Control Means;23rd AIAA Applied Aerodynamics Conference;2005-06-06

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