A hybrid Doublet Lattice-Doublet Point Method for general lifting surface configurations in subsonic flow

Author:

EVERSMAN WALTER1,PITT DALE2

Affiliation:

1. Missouri-Rolla, University, Rolla

2. McDonnell Aircraft Co., Saint Louis, MO

Publisher

American Institute of Aeronautics and Astronautics

Reference14 articles.

1. Spanwise-Dimensionless GP830Y1-kD Flgure 18. Comparisonof DLMforT-TallConfiguration Osciilatlng In YawAboutthe Mid-Chordof the Vertlcal Fln. SpanwlseDlstributlon of PltchlngMomentCoefficientonthe HorizontalTallPer UnRAngle

2. A doublet-lattice method for calculating lift distributions on oscillating surfaces in subsonic flows.

3. Application of the Doublet-Lattice Method to Nonplanar Configurations in Subsonic Flow

4. Refinement of the nonplanar aspects of the subsonic doublet-lattice lifting surface method.

5. Watkins, C., Runyan, H., and Woolston, D. "On the Kernel Function of the Integral Equation Relating the Lift and Downwash Distributions of Oscillating Finite Wings in Subsonic Flow," NACA Report 1234, 1955.

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