Wall Temperature and Rotation Rate Effects on the Magnus Force of a Spinning Rocket
Author:
Affiliation:
1. School of Aerospace Engineering, Beijing Institute of Technology, Beijing, P.R. China
2. Department of Engineering and Mathematics/MERI, Sheffield Hallam University, Sheffield, UK
Funder
National Science Foundation of China
Publisher
Informa UK Limited
Subject
Fluid Flow and Transfer Processes,Mechanical Engineering,Condensed Matter Physics
Link
https://www.tandfonline.com/doi/pdf/10.1080/01457632.2021.1905319
Reference23 articles.
1. C. H. Murphy and L. E. Schmidt, “The effect of length on the aerodynamic characteristics of bodies of revolution in supersonic flight,” U.S. Army Ballistics Research Laboratory, BRL-R-876, Aberdeen Proving Ground, MD, Aug. 1953.
2. L. E. Schmidt and C. H. Murphy, “The aerodynamic properties of the 7-caliber army-navy spinner rocket in transonic flight,” U.S. Army Ballistics Research Laboratory, BRL-MR-775, Aberdeen Proving Ground, MD, Mar. 1954.
3. W. Luchuk and W. Sparks, “Wind-tunnel magnus characteristics of the 7-caliber army-navy spinner rocket,” U.S. Naval Ordnance Laboratory, White Oak, MD, NAVORD Technical Report, No. 3813, 1954.
4. Numerical and Experimental Investigation of the Magnus Effect in Supersonic Flows
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