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Self-Adaptive Flight Control by Multivariable Parameter Identification
Author(s): Shipley, P. P., Engel, A. G., Jr., Hung, J. W.
Corporate Author(s): North American Aviation, Inc.
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1965-08
Report number: AFFDL TR 65-90
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Confac II, A General Computer Program for the Determination of Radiant-Interchange Configuration and Form Factors
Author(s): Toups, Kempton A.
Corporate Author(s): North American Aviation, Inc.
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1964-04
Report number: FDL TDR 64-43
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Matrix Error Analysis for Engineers
Author(s): Rosanoff, R. A., Ginsbur, T. A.
Corporate Author(s): North American Aviation, Inc.
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1966-11
Report number: AFFDL-TR-66-80 p. 887-910
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Sonic Fatigue Tolerance of Glass Filament Structure: Experimental Results
Author(s): Hayes, J. A.
Corporate Author(s): North American Aviation, Inc.
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1966-12
Report number: AFFDL TR 66-78
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A Regularization Method for Calculation of Stresses, Deformations, and Elastic Modes
Author(s): Falconer, Robert W., Lane, Robert D.
Corporate Author(s): North American Aviation, Inc.
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1966-11
Report number: AFFDL-TR-66-80 p. 191-204
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Structural Influence Coefficients for a Redundant System Including Beam-Column Effects
Author(s): Rodden, William P.
Corporate Author(s): North American Aviation, Inc.
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1966-11
Report number: AFFDL-TR-66-80 p. 353-383
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Modeling Techniques for Sonic Fatigue Prediction
Author(s): Wang, P.
Corporate Author(s): North American Aviation, Inc.
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1966-06
Report number: AFFDL TR 65-171