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Empirical Correlation of Excitation Environment and Structural Parameters with Flight Vehicle Vibration Response
Author(s): White, R. W., Bozich, D. J., Eldred, K. M.
Corporate Author(s): Northrup Corporation
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-12
Report number: AFFDL TR 64-160
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Design Guide for Bolted Joints in Composite Structures
Author(s): Ramkumar, R. L., Saether, E. S., Cheng, D.
Corporate Author(s): Northrup Corporation
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1986-03-01
Report number: AFWAL TR 86-3035
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Fracture Mechanics Guidelines for Aircraft Structural Applications
Author(s): Wilhelm, D. P.
Corporate Author(s): Northrup Corporation
Laboratory: Air Force Flight Dynamics Lboratory
Date of Publication: 1970-02
Report number: AFFDL TR 69-111
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Fatigue Testing of Honeycomb Sandwich Constructions
Author(s): Spector, H.
Corporate Author(s): Northrup Corporation
Laboratory: Directorate of Materials and Processes
Date of Publication: 1962-04
Report number: ASD TR 61-338

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