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The Use of a Flight Simulator for the Determination of a Maneuver Loads Spectrum
Author(s): None Given
Corporate Author(s): Douglas Aircraft Company, Inc.
Laboratory: Supersonic Transport Research Program
Date of Publication: 1964-07
Report number: ASD TDR 63-357
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Optimum Fatigue Spectra
Author(s): Neuls, G. S., Maier, H. G., Lerwick, T. R., Robb , E. A., Webster, I. J.
Corporate Author(s): Douglas Aircraft Company, Inc.
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1962-04
Report number: ASD TR 61-235
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Crack Strength and Crack Propagation Characteristics of High Strength Metals
Author(s): Christensen, R. H., Denke, P. H.
Corporate Author(s): Douglas Aircraft Company, Inc.
Laboratory: Directorate of Materials & Processes
Date of Publication: 1962-01
Report number: ASD TR 61-207
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Dynamic Modeling of Fuel Slosh
Author(s): Calkin, E. D., Webb, C. K.
Corporate Author(s): Douglas Aircraft Company, Inc.
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1964-03
Report number: RTD-TDR-63-4197 Part I, p. 417

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