Simultaneous Airframe and Propulsion Cycle Optimization for Supersonic Aircraft Design

Author:

Rallabhandi Sriram1,Mavris Dimitri1

Affiliation:

1. Georgia Institute of Technology

Publisher

American Institute of Aeronautics and Astronautics

Reference57 articles.

1. % Difference 84278 -11.46% 3084 -4.28% 2385 -0.42% 49996 0.00% 27908 7.49%

2. 0 167652 -4.60% 89438 -2.35%

3. 0 1463 0.00% 5026 8.30% 95926 -1.75% 9130 0.02% 1192 0.00% 1546 -11.64% 4301 19.58% 4542 -3.15% 2718 -27.04% 19825 -4.23% 5504 -1.00% 363 33.06% 49121 -2.01% 312700 -3.49%

4. 0 1463 0.00% 5026 8.30% 95926 -1.75% 9130 0.02% 1192 0.00% 1546 -11.64% 4301 19.58% 4542 -3.15% 2718 -27.04% 1896 -16.98% 367 0.00% 3318 -19.20% 1575 0.00%

5. 321506 -3.86%

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1. Design Guidelines for Supersonic Aircrafts in Civil Aviation;International Journal of Aviation, Aeronautics, and Aerospace;2019

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5. Effects of Advanced Engine Technology on Open Rotor Cycle Selection and Performance;Journal of Engineering for Gas Turbines and Power;2013-06-12

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