Prediction of unsteady aerodynamic loadings caused by leading edge and trailing edge control surface motions in subsonic compressible flow : analysis and results / W.S. Rowe [and others]

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Bibliographic Details
Online Access:	Search for the full-text version of this title in HathiTrust
Corporate Authors:	Boeing Commercial Airplane Company, Langley Research Center, United States. National Aeronautics and Space Administration
Other Authors:	Rowe, W. S.
Format:	Government Document Book
Language:	English
Published:	Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], [1975]
Series:	NASA contractor report ; NASA CR-2543.
Subjects:	Unsteady flow (Aerodynamics) > Computer simulation. Aerodynamic load > Computer simulation. Flutter (Aerodynamics) > Computer simulation. Leading edges (Aerodynamics) > Computer simulation. Airplanes > Control surfaces > Computer simulation. Compressibility > Computer simulation.

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Holdings details from Norlin Library - Government Information - US
Call Number:	NAS 1.26:2543
NAS 1.26:2543	Available Place a Hold