Robust Design Optimization of Two-Dimensional Scramjet Inlets-Reference-Cited by-同舟云学术

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Robust Design Optimization of Two-Dimensional Scramjet Inlets

Published:2006-06-15 Issue: Volume: Page:
ISSN:
Container-title:14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference
language:
Short-container-title:

Author:

Brown Matthew¹,Mudford Neil¹,Neely Andrew¹,Ray Tapabrata¹

Affiliation:

1. Australian Defence Force Academy

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2006-8140

Reference15 articles.

1. Seddon,J.,andGoldsmith,E.(1985).IntakeAerodynamics, Collins,London.

2. Optimization of Two-Dimensional Scramjet Inlets

3. Automated Design Optimization for the P2 and P8 Hypersonic Inlets

4. Paull,A.(2004)."NASAREPORTContractNo.L-71459D."UniversityofQueensland,Brisbane.

5. Physical and Computational Aspects of Convective Heat Transfer

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1. Scramjet Engine Flowpath That Improves Specific Impulse Using JP-7 Fuel;Journal of Propulsion and Power;2023-07

2. Lagrange Optimization of Shock Waves for Two-Dimensional Hypersonic Inlet with Geometric Constraints;Aerospace;2022-10-20

3. Robust Design Under Uncertainty of Hypersonic Inlets;AIAA AVIATION 2022 Forum;2022-06-20

4. Reduced Order Model Based on Gradient Optimization for Two Dimensional Scramjet Inlets;AIAA SCITECH 2022 Forum;2022-01-03

5. 2D Mixed-Compression Inlet Sizing of Supersonic Vehicles;AIAA AVIATION 2021 FORUM;2021-07-28

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