Spanwise Lift Distribution for Blended Wing Body Aircraft.
Author:
Affiliation:
1. University of Sheffield, Sheffield, England S1 3JD, United Kingdom
2. Cranfield University, Cranfield, England MK43 OAL, United Kingdom
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.4229
Reference20 articles.
1. Wing aerodynamics and the science of compromise
2. Flying wing—problems and decisions
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