Integration of Aerodynamic, Structural, Cost and Manufacturing Cosiderations During the Conceptual Design of a Thrust Reverser Cascade-Reference-Cited by-同舟云学术

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Integration of Aerodynamic, Structural, Cost and Manufacturing Cosiderations During the Conceptual Design of a Thrust Reverser Cascade

Published:2004-01-05 Issue: Volume: Page:
ISSN:
Container-title:42nd AIAA Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Butterfield Joseph¹,Yao Hui¹,Curran Richard¹,Price Mark¹,Armstrong Cecil¹,Raghunathan S.¹

Affiliation:

1. Queen's University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2004-282

Reference10 articles.

1. Saving costs in design, manufacturing and operation of aero engine parts

2. Sietzen F. "Call to Arms for an Ailing Industry". Aerospace America, American Institute of Aeronautics & Astronautics, March2003,pp30-34.

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1. Test Scheme Design and Numerical Simulation of Composite Thrust Reverser Cascade;Aerospace;2024-08-07

2. Progressive Failure Analysis of an Integral Composite Joint for Thrust Reverser Cascade;Key Engineering Materials;2019-03

3. A heuristic complexity-based method for cost estimation of aerospace systems;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2012-10-03

4. An integrated systems engineering approach to aircraft design;Progress in Aerospace Sciences;2006-06

5. Numerical Method for Cost-Weight Optimization of Stringer-Skin Panels;Journal of Aircraft;2006-01

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