Multipoint Design Optimization of Busemann-Based Intakes for Scramjet-Powered Ascent Flight-Reference-Cited by-同舟云学术

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Multipoint Design Optimization of Busemann-Based Intakes for Scramjet-Powered Ascent Flight

Published:2021-11 Issue:6 Volume:37 Page:850-867
ISSN:1533-3876
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Brahmachary Shuvayan¹^ORCID,Ogawa Hideaki¹^ORCID

Affiliation:

1. Kyushu University, Fukuoka 819-0395, Japan

Funder

Japan Society for the Promotion of Science

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.B38383

Reference32 articles.

1. Scramjet Engines: The First Forty Years

2. Hypersonic Airbreathing Propulsion

3. Flight Data Analysis of the HyShot 2 Scramjet Flight Experiment

4. Preliminary X-43 flight test results

5. Supersonic Combustion in Air-Breathing Propulsion Systems for Hypersonic Flight

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1. Hypersonic inlet flow field reconstruction dominated by shock wave and boundary layer based on small sample physics-informed neural networks;Aerospace Science and Technology;2024-07

2. Design space investigations of scramjet engines using reduced-order modeling;Acta Astronautica;2024-04

3. Recent advances and prospects in hypersonic inlet design and intelligent optimization;Aerospace Science and Technology;2024-03

4. Prospects for scramjet engines in reusable launch applications: A review;International Journal of Hydrogen Energy;2023-11

5. Flow field reconstruction in inlet of scramjet at Mach 10 based on physical information neural network;Physics of Fluids;2023-10-01

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