Hypersonic flow over a multi-step afterbody

Author:

Menezes V.,Kumar S.,Maruta K.,Reddy K. P. J.,Takayama K.

Publisher

Springer Science and Business Media LLC

Subject

General Physics and Astronomy,Mechanical Engineering

Cited by 20 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 blunt body in hypersonic regime using afterbody modifications;INTELLIGENT BIOTECHNOLOGIES OF NATURAL AND SYNTHETIC BIOLOGICALLY ACTIVE SUBSTANCES: XIV Narochanskie Readings;2023

2. Flow modification cooling technique to reduce aerodynamic wave drag by mechanical cut shape aero-spike for the blunted body at Mach 8.0;APPLIED DATA SCIENCE AND SMART SYSTEMS;2023

3. Numerical investigation of hypersonic flow over 60 degree apex angle blunted cone with flat aerodisk spike: A flow modification technique;2ND INTERNATIONAL CONFERENCE & EXPOSITION ON MECHANICAL, MATERIAL, AND MANUFACTURING TECHNOLOGY (ICE3MT 2022);2023

4. Universal scaling parameter for a counter jet drag reduction technique in supersonic flows;Physics of Fluids;2020-03-01

5. Hypersonic flow past a spherically blunted nose cone: a computational study;Progress in Computational Fluid Dynamics, An International Journal;2020

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