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Multidisciplinary Design and Prototype Development of a Very Small Remotely-Piloted Reconnaissance Airplane Mississippi State Univ

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Raise-Rohani, Masoud, author.
Conference Name:
World Aviation Congress & Exposition (1997-10-13 : Anaheim, California, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1997
Summary:
The multidisciplinary design optimization (MDO) methodology is employed for the design of a very small remotely-piloted airplane for a reconnaissance mission. The airplane configuration established at the conceptual design level is optimized for minimum size subject to performance, stability, weight, and dimension constraints. The constrained optimization problem is solved using the extended interior penalty function method based on finite-difference approximations of the sensitivity derivatives. The MDO-based design is validated both analytically and through the development and flight testing of a prototype airplane
Notes:
Vendor supplied data
Publisher Number:
975547
Access Restriction:
Restricted for use by site license

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