Experimental Investigation of Base-Drag Reduction via Boundary-Layer Modification
Author:
Affiliation:
1. Department of Mechanical Engineering, University of Wyoming, Laramie, Wyoming 82072
2. Department of Mechanical Engineering, Utah State University, Logan, Utah 84332
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J051825
Reference27 articles.
1. HoernerS. F., Fluid Dynamic Drag, Self-Published, Midland Park, NJ, 1965, pp. 3.17–3.20.
2. SaltzmanE. J.WangK. C.IliffK. W. “Flight Determined Subsonic Lift and Drag Characteristics of Seven Lifting-Body and Wing-Body Re-Entry Vehicle Configurations With Truncated Bases,” AIAA Paper 1999-0383, 1999.
3. A base drag reduction experiment on the X-33 linear aerospike SR-71 experiment (LASRE) flight program
4. Drag Reduction on Blunt-Based Vehicles Using Forebody Surface Roughness
5. DeckerR. K. “Viscous Drag Measurement and Its Application to Base Drag Reduction,” Master’s Thesis, Univ. of Wyoming, Laramie, WY, May 2002.
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