Design of a Variable Camber Flap for Minimum Drag and Improved Energy Efficiency-Reference-Cited by-同舟云学术

Design of a Variable Camber Flap for Minimum Drag and Improved Energy Efficiency

Published:2009-05-04 Issue: Volume: Page:
ISSN:
Container-title:50th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
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Author:

Marques Marco¹,Gamboa Pedro¹,Andrade Edi¹

Affiliation:

1. University of Beira Interior

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2009-2196

Reference23 articles.

1. Optimization of a Morphing Wing Based on Coupled Aerodynamic and Structural Constraints

2. 2Gamboa, P. V. "Multidisciplinary Design Optimization of Morphing Aircraft", PhD Thesis,Departamento de Ciências Aeroespaciais,UniversidadedaBeiraInterior,December2007.

3. Actuator-Work Concepts Applied to Unconventional Aerodynamic Control Devices

4. Civil-Transport Wing Design Concept Exploiting New Technologies

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