A finite-step method for calculation of theoretical load distributions for arbitrary lifting surface arrangements at subsonic speeds. Blackwell, J. A. Technical Report NASA Langley Research Center, Hampton, VA, 1969.
Paper abstract bibtex Load distribution calculations for subsonic compressible flow of arbitrary wings and lifting surfaces
@techreport{blackwell_finite-step_1969,
address = {Hampton, VA},
title = {A finite-step method for calculation of theoretical load distributions for arbitrary lifting surface arrangements at subsonic speeds},
url = {http://hdl.handle.net/2060/19690021959},
abstract = {Load distribution calculations for subsonic compressible flow of arbitrary wings and lifting surfaces},
institution = {NASA Langley Research Center},
author = {Blackwell, J. A.},
year = {1969},
}
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