Supersonic Flow Field Characteristics of a Sharp Spiked Blunt Body Having Various Nose Cone Fairings

Author:

Sarwar MD. G.,Kumar P.,Das S.

Publisher

Springer Nature Singapore

Reference15 articles.

1. Huang W (2015) A survey of drag and heat reduction in supersonic flows by a counterflowing jet and its combinations. J Zhejiang Univ-Sci A 16(7):551–561. https://doi.org/10.1631/jzus.A1500021

2. John B, Kulkarni V (2015) Review of drag reduction techniques for hypersonic flows. Int J Appl Eng Res 10(18):39488–39495

3. Sidney R (1947) Alexander, results of tests of determine the effect of a conical windshield on the drag of a bluff body at supersonic speeds. National Aeronautics and Space Administration Hampton Va Langley Research Center, RM-No-L6K08a.

4. Karimi MS, Oboodi MJ (2019) Investigation and recent developments in aerodynamic heating and drag reduction for hypersonic flows. Heat Mass Transf 55(2):547–569. https://doi.org/10.1007/s00231-018-2416-1

5. Crawford DH (1959) Investigation of the flow over a spiked-nose hemisphere-cylinder at a Mach number of 6.8. National Aeronautics and Space Administration, TN-D-118. https://dp.la/item/e1de7b2f860151cea4f64f4ee1a6ef4d

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