Determination of the aerodynamic characteristics of the mission adaptive wing
Author:
Affiliation:
1. Air Force Flight Test Center, Edwards Air Force Base, California
2. Boeing Advanced Systems, Seattle, Washington
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.45965
Reference6 articles.
1. Analysis and design of wing-body combinations at subsonic and supersonic speeds.
2. Determination of the aerodynamic characteristics of the Mission Adaptive Wing
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