Identification of an error in the distribution of the NASA model AP-8 MIN

Abstract

References 1 Moore, F. G., Hymer, T. C, and Mclnville, R. M., Improved Aeroprediction Code: Part I—Summary of New Methods and Comparison with Experiment, Naval Surface Warfare Center Dahlgren Division, NSWCDD/TR93/91, Dahlgren, VA, May 1993. Moore, F. G., Mclnville, R. M., and Hymer, T. C., Improved Aeroprediction Code: Part II—Computer Program User's Guide and Listing, Naval Surface Warfare Center Dahlgren Division, NSWCDD/TR-93/241, Dahlgren, VA, Aug. 1993. Moore, F. G., Hymer, T. C., and Mclnville, R. M., A Planar Nonlinear Missile Aeroprediction Code for all Mach Numbers, AIAA Paper 94-0026, Jan. 1994. Fidler, J. E., and Bateman, M. C., Methods for High Incidence Missile Design, Journal of Spacecraft and Rockets, Vol. 12, No. 3, 1975, pp. 162-168. Moore, F. G., and Mclnville, R. M., A New Method for Calculating WingAlone Aerodynamics to Angle of Attack 180 deg, Naval Surface Warfare Center Dahlgren Division, NSWCDD/TR-94/3, Dahlgren, VA, March 1994. Stallings, R. L., Jr., and Lamb, M., Wing-Alone Aerodynamic Characteristics for High Angles of Attack at Supersonic Speeds, NASA Technical Paper 1889, July 1981. Baker, W. B., Jr., Static Aerodynamic Characteristics of a Series of Generalized Slender Bodies with and without Fins at Mach Numbers from 0.6 to 3.0 and Angles of Attack from 0 to 180 deg, Arnold Engineering Development Center, TR-75-124, Vols. I and II, Tullahoma, TN, May 1976. Nielsen, J. N., Hemsch, M. J., and Smith, C. A., A Preliminary Method for Calculating the Aerodynamic Characteristics of Cruciform Missiles to High Angles of Attack Including Effects of Roll Angle and Control Deflections, Office of Naval Research, Report ONR-CR215-216,4F, Arlington, VA, Nov. 1977.