Civil-Transport Wing Design Concept Exploiting New Technologies-Reference-Cited by-同舟云学术

Civil-Transport Wing Design Concept Exploiting New Technologies

Published:2006-07 Issue:4 Volume:43 Page:932-940
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Edi Prasetyo¹,Fielding J. P.²

Affiliation:

1. University Putra Malaysia, Selangor DE. 43400, Malaysia

2. Cranfield University, Cranfield, England MK43 0AL, United Kingdom

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.15556

Reference19 articles.

1. 3Edi, P. "Investigation of the Application of Hybrid Laminar Flow Control and Variable Camber Wing Design for Regional Aircraft," Ph.D. Dissertation,AVT/CoA/Cranfield Univ., Cranfield, England, U.K., Sept. 1998.

2. 4Boeing Commercial Airplane Co. "Hybrid Laminar Flow Control Study Final Technical Report," NASACR165930,Oct. 1982.

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