Design of a Supersonic Natural Laminar Flow Wing-Body
Author:
Affiliation:
1. Italian Aerospace Research Center, 81041 Capua, Italy
2. ONERA, 92190 Paris, France
3. ONERA, 31055 Toulouse, France
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C031039
Reference59 articles.
Cited by 9 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
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2. Effect of Wing Pressure Distribution on Sonic-Boom Intensity of Supersonic Transport Aircrafts;Lecture Notes in Electrical Engineering;2024
3. Assessment of Potential Commercial Success of Business Jets with Natural Laminar Flow;Journal of Aircraft;2023-03
4. The Objective Space and the Formulation of Design Requirement in Natural Laminar Flow Optimization;Applied Sciences;2020-08-27
5. UQ Sensitivity Analysis and Robust Design Optimization of a Supersonic Natural Laminar Flow Wing-Body;Uncertainty Management for Robust Industrial Design in Aeronautics;2018-07-21
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