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Thermal Effects On Static Aeroelastic Stability And Control. Description and Results of Tests Conducted to Determine the Thermally Affected Deflectional Behavior of Corrugated Multiweb Wing Structures
Author(s): Quinn, James F., Turrentine, Donald, Gallagher, Richard H.Corporate Author(s): Fligth Control Laboratory
Laboratory: Flight Control Laboratory
Date of Publication: 1959-11
Report number: WADD TR 60-229
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Supersonic Aeroelastic Effects On Static Stability And Control, Part II - Structures
Author(s): Rattinger, Ivan, Gallagher, Richard H.Corporate Author(s): Bell Aircraft Corporation
Laboratory: Flight Control Laboratory
Date of Publication: 1960-04
Report number: WADC TR 58-95 Part 2
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Measurement of Angular Displacements of Practical Wing Structures by the Moire' Fringe Technique
Author(s): Padlog, Joseph, Gallagher, Richard H.Corporate Author(s): Bell Aerosystems Company
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-09
Report number: FDL TDR 64-42
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Nonlinear Thermoelastic Effects on Hypersonic Stability and Control: Part II, Analytical and Experimental Statis Aerothermoelasticity
Author(s): Batt, James R., Gallagher, Richard H.Corporate Author(s): Bell Aerosystems Company
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-10
Report number: FDL TDR 64-16 Part 2
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Thermoelastic Effects on Hypersonic Stability and Control: Part II - Volume III: Elastic Response Analysis of Fuselage and Combined Wing-Fuselage Structures
Author(s): Huff, Rolland D., Gallagher, Richard H.Corporate Author(s): Bell Aerosystems Company
Laboratory: Flight Control Laboratory
Date of Publication: 1963-05
Report number: ASD TR 61-287 Part 2 Volume 3
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Thermoelastic Effects on Hypersonic Stability and Control: Part II - Volume I Elastic Response Determinations for Severely Heated Wings
Author(s): Gallagher, Richard H., Huff, Rolland D.Corporate Author(s): Bell Aerosystems Co.
Laboratory: Flight Control Laboratory
Date of Publication: 1962-08
Report number: ASD TR 61-287 Part 2 Volume 1
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Development of Advanced Structural Optimization Programs and their Application to Large Order Systems
Author(s): Gellatly, Ronald A., Gallagher, Richard H.Corporate Author(s): Textron's Bell Aerospace Company
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1966-11
Report number: AFFDL-TR-66-80 p. 231-251
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Elastic Instability Predictions for Doubly-Curved Shells
Author(s): Gallagher, Richard H., Yang, Henry T. Y.Corporate Author(s): Cornell University
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1969-12
Report number: AFFDL TR 68-150 p. 711-739
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A Procedure for Finite Element Plate and Shell Pre- and Post-Buckling Analysis
Author(s): Gallagher, Richard H., Lien, S., Mau, S. T.Corporate Author(s): Cornell University
Date of Publication: 1973-12
Report number: AFFDL TR 71-160 p. 857-879
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- Gallagher, Richard H. (9)
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