Numerical evaluation of aerodome and cooling jet for aeroheating reduction-Reference-Cited by-同舟云学术

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Numerical evaluation of aerodome and cooling jet for aeroheating reduction

Published:2019-03 Issue: Volume:86 Page:520-533
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Qin Qihao,Xu Jinglei

Funder

NSFC

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference54 articles.

1. Numerical investigation of a spiked blunt nose cone at hypersonic speeds;Gauer;J. Spacecr. Rockets,2008

2. Effect of the injector configuration for opposing jet on the drag and heat reduction;Li;Aerosp. Sci. Technol.,2016

3. Survey of aerodynamic drag reduction at high speed by energy deposition;Knight;J. Propuls. Power,2008

4. Numerical study of novel drag reduction techniques for hypersonic blunt bodies;Marley;AIAA J.,2011

5. Recent advances in the aerothermodynamics of spiked hypersonic vehicles;Ahmed;Prog. Aerosp. Sci.,2011

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1. Heat and drag reduction on the hypersonic nose with a nexus between active and passive control methods;Physics of Fluids;2024-01-01

2. Evaluation of Various Flow Control Methods in Reducing Drag and Aerodynamic Heating on the Nose of Hypersonic Flying Objects;Journal of Applied Fluid Mechanics;2024-01-01

3. Comparison of single and multi-coolant axial jets on the temperature reduction of nose cone with multiple-row disk;Results in Engineering;2023-12

4. Study on Ground Experimental Method of Stagnation Point Large Heat Flux of Typical Sharp Wedge Leading Edge Structure;Aerospace;2023-10-06

5. Investigation of influence factors to the reduction of hypersonic blunt-body drag and aeroheating based on a spike - aerodisk - Channel concept;Acta Astronautica;2023-10

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