Physical properties of Maskell's induced drag integral
Author:
Affiliation:
1. Boeing Co., Seattle, WA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2001-421
Reference12 articles.
1. Maskell, E. C. "Progress Towards a Method for the Measurement of the Components of the Drag of a Wing ofFinite Span," RAETechnical Report 72232, 1972.
2. Quantitative low-speed wake surveys
3. Quantitative wake surveys behind a tractor propeller-wing configuration
4. Airplane Flow-Field Measurements
5. Development of a universal wake survey data analysis code
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