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A Theoretical And Experimental Investigation Of The Acoustic Response Of Cavities In An Aerodynamic Flow
Author(s): Plumblee, H. E., Lassiter, L. W., Gibson, J. S.Corporate Author(s): Flight Dynamics Laboratory
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1962-03
Report number: WADD TR 61-75
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Structural Flight Loads Data from F-106A Aircraft
Author(s): Vahldiek, Artie, Monfort, John B.Corporate Author(s): Flight Dynamics Laboratory
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1962-02
Report number: ASD TDR 62-246
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The Evolution of USAF Environmental Testing
Author(s): Junker, V. J.Corporate Author(s): Flight Dynamics Laboratory
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1965-10
Report number: AFFDL TR 65-197
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Feasibility Studies on Use of Artrons as Logic Elements in Flight Control Systems
Author(s): Mirabelli, R. E., Connelly, E. M., Worthen, J. E.Corporate Author(s): Flight Dynamics Laboratory
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1964-09
Report number: FDL TDR 64-23
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A Source-Doublet Approach to Modeling Triple Ejector Rack Store Configurations and Force Calculations
Author(s): Dyer, Calvin L., Heath, Charles B.Corporate Author(s): Flight Dynamics Laboratory
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1981-07-01
Report number: AFWAL TR 81-3059
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Table of Contents
Corporate Author(s): Flight Dynamics LaboratoryLaboratory: Flight Dynamics Laboratory
Date of Publication: 1989-11-01
Report number: WRDC-TR-89-3116 Volume III p. 1
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