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Application of the Created Response Surface Technique to Structural Optimization
Author(s): Marcal, Pedro V., Gellatly, Ronald A.Corporate Author(s): Boeing Company
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1969-12
Report number: AFFDL TR 68-150 p. 83-110
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Compatibility of Tankage Materials with Liquid Propellants
Author(s): Tiffany, C. F., Lorenz, P. M.Corporate Author(s): Boeing Company
Laboratory: Air Force Materials Laboratory
Date of Publication: 1969-05
Report number: AFML TR 69-99
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Low Altitude Atmospheric Turbulence Lo-Locat Phase III Interim Report: Volume II. Instrumentation and Data Processing Details, Gust Velocity Data, and Test Log
Author(s): Monson, K. R., Mielke, R. H., et al., Jones, G. W.Corporate Author(s): Boeing Company
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1969-10
Report number: AFFDL TR 69-63 Volume 2
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Finite Elements in Linear Viscoelasticity
Author(s): White, J. L.Corporate Author(s): Boeing Company
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1969-12
Report number: AFFDL TR 68-150 p. 489-516
full text available
Some Applications of Finite Analysis to Shell Buckling Prediction
Author(s): Backus, Walter E.,, Mello, Raymond M.Corporate Author(s): Boeing Company
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1969-12
Report number: AFFDL TR 68-150 p. 869-893
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