Improvement of the Newtonian Method to Estimate Supersonic Vehicle Drag
Publication: Journal of Aerospace Engineering
Volume 28, Issue 5
Abstract
A simple, easy-to-use method to compute vehicle drag at low and moderate supersonic speeds is presented in this study. A novel version of the Newtonian sine-squared law is proposed and used to compute supersonic pressure or wave drag for various geometries. The new version implicitly includes shockwave contribution not present in the original law. The results obtained are compared with the those found in the literature and discussed in order to estimate the applicability and validity of the method. The method’s suitability for optimization purposes is also briefly considered.
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References
Ames Research Center. (1953). “Equations, tables and charts for compressible flow.”, Naval Air Station, Moffett Field, Mountain View, CA.
Anderson, J. D., Jr. (1990). Modern compressible flow with historical perspective, 2nd Ed., McGraw-Hill Aerospace Series, New York.
Bailey, A. B., and Hiatt, J. (1971). “Free-flight measurement of sphere drag at subsonic, transonic, supersonic and hypersonic speeds for continuum, transition and near-free-molecular flow conditions.”, ARO, Arnold AFB, TN.
Chieh, T. W. (2010). “Aerodynamic validation of emerging projectile and missile configurations.” Master thesis, Naval Postgraduate School, Monterey, CA.
DeSpirito, J., and Heavey, K. R. (2004). “CFD computation of magnus moment and roll damping moment of a spinning projectile.” AIAA-2004-4713, AIAA Atmospheric Flight Mechanics Conf. and Exhibit, AIAA, Reston, VA.
Giraud, M., Berner, C., and Winchenbach, G. (1996). “Aeroballistic investigation of supersonic hemispheric shapes computations and experiments.” ADPA, 16th Int. Symp. on Ballistics, Arlington, VA.
Hemsch, M. J., ed. (1992). “Tactical missile aerodynamics: General topics.” Progress in astronautics and aeronautics series, Vol. 141, AIAA, Reston, VA.
Hoerner, S. F. (1965). Fluid-dynamic drag, Bricktown, NJ.
Jorgensen, L. H. (1973). “Prediction of static aerodynamic characteristics for space-shuttle-like and other bodies at angles of attack from 0° to 180°.”, Ames Research Center, Mountain View, CA.
Liepmann, H. W., and Roshko, A. (1962). Elements of gasdynamics, John Wiley & Sons, Calcit Aeronautical Series, Fourth Printing, Hoboken, NJ.
McCoy, R. (1981). “MC DRAG—A computer program for estimating the drag coefficients of projectiles, final report.” U.S. Army Ballistic Research Laboratory, Aberdeen Proving Ground, Aberdeen, MD.
McCoy, R. (1988). “The aerodynamic characteristics of 7.62 mm match bullets.”, U.S. Army Ballistic Research Laboratory, Aberdeen Proving Ground, Aberdeen, MD.
Moore, F. G. (2000). “Approximate methods for weapon aerodynamics.” Progress in astronautics and aeronautics series, Vol. 186, AIAA, Reston, VA.
Nielsen, J. N. (1960). Missile aerodynamics, McGraw-Hill Book Company Series in Missile and Space Technology, New York.
Perkins, E. W., Jorgensen, L. H., and Sommer, S. C. (1958). “Investigation of the drag of various axially symmetric nose shapes of fineness ratio 3 for Mach numbers from 1.24 to 7.4.”, Naval Air Station, Moffett Field, Mountain View, CA.
Sahu, J. (1986). “Drag prediction for projectiles at transonic and supersonic speeds.”, U.S. Army Ballistic Research Laboratory, Aberdeen Proving Ground, Aberdeen, MD.
Tanner, M. (1984). “Steady base flows.” Prog. Aerosp. Sci., 21(2), 81–157.
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© 2014 American Society of Civil Engineers.
History
Received: Apr 16, 2014
Accepted: Jul 16, 2014
Published online: Sep 2, 2014
Discussion open until: Feb 2, 2015
Published in print: Sep 1, 2015
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