Drag of circular cylinders at transonic mach numbers

Journal of Aircraft

Volumn 14, Issue 6, 1977, Pages 605-607

  Macha, John M ^a  

^a TEXAS A AND M UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 85003283005     PISSN: 00218669     EISSN: None     Source Type: Journal    
DOI: 10.2514/3.58828     Document Type: Article

References (8)

1. Jorgensen, L. H., “Prediction of Static Aerodynamic Characteristics for Space-Shuttle-Like and Other Bodies at Angles of Attack from 0 Degrees to 180 Degrees,” NASATN D-6996, Jan. 1973.
2. Knowler, A. E. and Pruden, F. W., “On the Drag of Circular Cylinders at High Speeds,” British Aeronautics Research Council, R&M No. 1933,1944.
3. Matt, H., “Measurement of Drag of Round Rods of Various Diameters at High Subsonic Airspeed,” Deutsche Luftfahrtforschung, Forschungsberichte (Report) No. 1825, 1943;
4. Naumann, A. and Pfeifer, H., “Uber Die Grenz-schichtstromung am Zylinder bei hohen Geschwindigkeiten,” Advances in Aeronautical Sciences, Vol. 3, edited by Th. von Karman, Pergamon Press, New York, 1962, pp. 185-206.
5. Welsh, C. J., “The Drag of Finite Length Cylinders Determined from Flight Tests at High Reynolds Numbers for a Mach Numbers Range from 0.51o 1.3,” NACA TN 2491, June 1973.
6. Macha, J. M., “A Wind-Tunnel Investigation of Circular and Straked Cylinders in Transonic Cross Flow,” Texas A&M Research Foundation, College Station, Texas, Rept. 3318-76-01, Nov. 1976.
7. Gowen, F. E. and Perkins, E. W., “Drag of Circular Cylinders for a Wide Range of Reynolds Numbers and Mach Numbers, NACA TN 2960, June 1953.
8. Jorgensen, L. H., “A Method for Estimating Static Aerodynamic Characteristics for Slender Bodies of Circular and Noncircular Cross Section Alone and with Lifting Surfaces at Angles of Attack from 0 Degrees to 90 Degrees,” NASATN D-7228, April 1973