Approach to Determine the Most Efficient Supersonic Mach Number
References
[1] , Elements of Gasdynamics, Wiley, New York, 1957, Chaps. 2, 4.
[2] , The Dynamics and Thermodynamics of Compressible Fluid Flow, Vol. I, The Ronald Press Company, New York, 1953, Chaps. 5, 10, 16.
[3] , Fundamentals of Aerodynamics, 6th ed., McGraw–Hill Education, New York, 2017, Chaps. 1, 8, 9.
[4] , A Case Study by Aerospatiale and British Aerospace on the Concorde,
AIAA Professional Study Series , AIAA, Reston, VA, 1980, Sec. 3.[5] , “Exploring the Prospect of Small Supersonic Airliners—A Case Study Based on the Aerion AS2 Jet,” AIAA Paper 2017-3588, June 2017.
[6] , Fluid Mechanics, 2nd ed., Pergamon Press, New York, 1987, pp. 363–364.
[7] , “Theoretical Solutions and Physical Significances for Minimum Ratio of Total Pressure Loss by Oblique Shock,” Acta Aeronautica et Astronautica Sinica, Vol. 39, No. 12, 2018, Paper 122517. https://doi.org/10.7527/S1000-6893.2018.22517
[8] , Molecular Gas Dynamics and the Direct Simulation of Gas Flows, Oxford Univ. Press, London, 1994, Chaps. 2, 14.
[9] , “Nonequilibium Entropy in as Shock,” Entropy, Vol. 19, No. 7, 2017, pp. 368. https://doi.org/10.3390/e19070368
[10] , “The Conical Shock Wave Formed by a Cone Moving at a High Speed,” Proceedings of the Royal Society of London. Series A, Mathematical and Physical Sciences, Vol. 159, No. 898, 1937, pp. 459–472.
[11] , Compressible Fluid Dynamics, Maple Press, Boulder, CO, 1988, Chap. 10.