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.
A finite-step method for calculation of theoretical load distributions for arbitrary lifting surface arrangements at subsonic speeds [link]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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