NASA NTRS · 19690021959
A finite-step method for calculation of theoretical load distributions for arbitrary lifting surface arrangements at subsonic speeds
Abstract
Load distribution calculations for subsonic compressible flow of arbitrary wings and lifting surfaces
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Blackwell, J. A., Jr.. 1969-07-01. A finite-step method for calculation of theoretical load distributions for arbitrary lifting surface arrangements at subsonic speeds. https://ntrs.nasa.gov/citations/19690021959
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