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- [3] Viscous contribution to the high Mach number damping in pitch of blunt slender cones at small angles of attack Khalid, M., 1600, Royal Aeronautical Soc, London, United Kingdom (99):
- [4] VISCOUS CONTRIBUTION TO THE HIGH MACH NUMBER DAMPING IN PITCH OF BLUNT SLENDER CONES AT SMALL ANGLES OF ATTACK AERONAUTICAL JOURNAL, 1995, 99 (982): : 69 - 74
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- [8] Strakes Effects on Asymmetric Flow Over a Blunt-Nosed Slender Body at a High Angle of Attack JOURNAL OF FLUIDS ENGINEERING-TRANSACTIONS OF THE ASME, 2019, 141 (06):
- [9] APPROXIMATE METHOD TO CALCULATE MACH NUMBER-DISTRIBUTION ON SPHERICALLY CAPPED CONES AT ZERO ANGLE OF ATTACK IN SUPERSONIC-FLOW ZEITSCHRIFT FUR FLUGWISSENSCHAFTEN, 1974, 22 (11): : 372 - 379