Spanload optimization for strength designed lifting surfaces-Reference-Cited by-同舟云学术

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Spanload optimization for strength designed lifting surfaces

Published:1988-06-06 Issue: Volume: Page:
ISSN:
Container-title:6th Applied Aerodynamics Conference
language:
Short-container-title:

Author:

CRAIG ANTHONY¹,MCLEAN J.¹

Affiliation:

1. Boeing Commercial Airplanes, Seattle, WA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1988-2512

Reference9 articles.

1. Munk,M. 'MinimumInduced Dragof Airfoils', NACATR 121,1921.

2. Jones,R. 'The Spanwise Distribution of Lift for Minimum Induced Dragof Wings Having GivenLift and Root Bending Moment', NACATN-2249,1950.

3. Jones,R. and Lasinski,T.'Effect of Wingletson the Induced Drag of IdealWing Shapes', NASATM-81230,1980.

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2. Comparison of Theoretical and Multifidelity Optimum Aerostructural Solutions for Wing Design;Journal of Aircraft;2022-01

3. Low-fidelity method for rapid aerostructural optimisation and design-space exploration of planar wings;The Aeronautical Journal;2021-04-30

4. Comparison of Theoretical and High-Fidelity Aerostructural Solutions;AIAA Scitech 2021 Forum;2021-01-04

5. Minimum Induced Drag for Tapered Wings Including Structural Constraints;Journal of Aircraft;2020-07

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