Computational Investigations Aerodynamic Forces at Supersonic / Hypersonic Flow past a Blunt Body with various Forward Facing Spikes-Reference-Cited by-同舟云学术

Computational Investigations Aerodynamic Forces at Supersonic / Hypersonic Flow past a Blunt Body with various Forward Facing Spikes

Published:2004-06-20 Issue: Volume: Page:
ISSN:
Container-title:22nd Applied Aerodynamics Conference and Exhibit
language:
Short-container-title:

Author:

Asif Muhammad¹,Zahir Salimuddin¹,Kamran Nasir¹,Khan Mahmood¹

Affiliation:

1. CFD Society

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2004-5189

Reference10 articles.

1. Influence of Spike Shape at Supersonic Flow Past Blunt-Nosed Bodies: Experimental Study

2. Carwford, D. J. "Hypersonic Flow over a spiked-None Hemisphere Cylinder at a Mach Number of 6.8," NASA TN D-118, Dec.1959.3Mehta,R.C."NumericalheatTransferStudyoverSpikedBluntBodiesatMach6.8",AIAAPaper,May2000.

3. 4Yamauchi,M.,Fujii.,K.Tamura,Y.,andHigashinoF."NumericalinvestigationofsupersonicFlowsAroundaSpikedBluntBody," AIAA Paper 93-0887,Jan.1973.

4. Transonic flow modes of an axisymmetric blunt body

Cited by 9 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Drag Reduction of a Hemispherical Body Adopting Spike at Supersonic Speed;Journal of Aerospace Sciences and Technologies;2023-08-15

2. Review of wave drag reduction techniques: Advances in active, passive, and hybrid flow control;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2022-03-12

3. Evaluation of aerospike for drag reduction on a blunt nose using experimental and numerical modeling;Acta Astronautica;2019-07

4. Numerical Simulation of Aerodynamic Heating over Solid Blunt Configuration with Porous Spike;Journal of Aerospace Engineering;2018-11

5. Spike Effects on Drag Reduction for Hypersonic Lifting Body;Journal of Spacecraft and Rockets;2017-11