Design Optimization of a Class of Low Reynolds, High Mach Number Airfoils for Use in the Martian Atmosphere-Reference-Cited by-同舟云学术

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Design Optimization of a Class of Low Reynolds, High Mach Number Airfoils for Use in the Martian Atmosphere

Published:2005-06-06 Issue: Volume: Page:
ISSN:
Container-title:23rd AIAA Applied Aerodynamics Conference
language:
Short-container-title:

Author:

Fuhrmann Henri¹

Affiliation:

1. Orbital Sciences Corporation

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2005-4603

Reference41 articles.

1. A concept Study of a Remotely Piloted Vehicle for Mars Exploration. NASA CR-157942,1978.

2. Guynn, M. D., Croom, M. A., Smith, S. C., Parks, R. W., Gelhausen, P. A. Evolution of a Mars Airplane Concept for the ARES Mars Scout Mission. AIAAPaperNo.2003-6578,September,2003.

Cited by 2 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

1. An evolutionary geometric primitive for automatic design synthesis of functional shapes: The case of airfoils;Advances in Engineering Software;2014-01

2. Application of Swarm Approach and Artificial Neural Networks for Airfoil Shape Optimization;12th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference;2008-06-14

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