Prediction of Span Loading from Measured Wake-Vortex Structure -An Inverse Betz Method
Author:
Affiliation:
1. NASA Ames Research Center, Moffett Field, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.59845
Reference10 articles.
1. Verhalten von Wirbelsystemen
2. On the Inviscid Rolled-Up Structure of Lift-Generated Vortices
3. A method of calculating aircraft wake velocity profiles and comparison with full-scale experimental measurements
4. Structure of Betz Vortex Cores
5. Theoretical Study of Lift-Generated Vortex Wakes Designed to Avoid Rollup
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1. Wake vortex characteristics of transport aircraft;Progress in Aerospace Sciences;2011-02
2. Application of Vortex Invariants to Roll Up of Vortex Pairs;Journal of Aircraft;2004-09
3. Lift-generated vortex wakes of subsonic transport aircraft;Progress in Aerospace Sciences;1999-08
4. Extended-Betz Methods for Roll-Up of Vortex Sheets;Journal of Aircraft;1997-09
5. Vortex structures and span loadings from alleviated-wake measurements;15th Applied Aerodynamics Conference;1997-06-23
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