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Mehtods For Predicting Aeroelastic Effects On Subsonic Static Longitudinal Stability Of Aircraft
Author(s): Paraghamian, B., Lohman, R. L.Corporate Author(s): Dept. Of Aerodynamics, Martin Company
Laboratory: Aircraft Laboratory
Date of Publication: 1954-09
Report number: WADC TR 54-265
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The Effects Of Thermal Radiation On Aircraft Structures, Part I. The M.I.T. Mark I Radiant Heating Structural Test Facility
Author(s): Loria, John C., Mar, James W., Blackstock, William J.Corporate Author(s): Massachusetts Institute of Technology
Laboratory: Aircraft Laboratory
Date of Publication: 1954-10
Report number: WADC TR 54-384 Part 1
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Analytical Studies Of Aircraft Structures Exposd To Transient External Heating Volume I Thermal Response Of A "Thin" Plate Under Influence Of A Constant Temperature Edge
Author(s): Ambrosio, Alphonso, Ishimoto, TakaoCorporate Author(s): University Of California, Department Of Engineering
Laboratory: Aircraft Laboratory
Date of Publication: 1954-05
Report number: WADC TR 54-579 Volume 1
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Analytical Studies Of Aircraft Structures Exposed To Transient External Heating. Vol. II: Thermal Response Of A Finite Plate And The "thin" Plate Criterion
Author(s): Ambrosio, Alphonso, Ishimoto, TakaoCorporate Author(s): University Of California, Department Of Engineering
Laboratory: Aircraft Laboratory
Date of Publication: 1954-11
Report number: WADC TR 54-579 Volume 2
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Subsonic Flutter Tests of an Unswept All-Movable Horizontal Tail
Author(s): Hoffman, Niles R., Spielberg, Irvin N.Corporate Author(s): Aircraft Laboratory
Laboratory: Aircraft Laboratory
Date of Publication: 1954-03
Report number: WADC TR 54-53
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Theoretical Studies of the Effects of Aspect Ratio on Flutter
Author(s): Goland, Martin, Luke, Y. L., Dengler, M. A.Corporate Author(s): Midwest Research Institute
Laboratory: Aircraft Laboratory
Date of Publication: 1954-06
Report number: WADC TR 54-29
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Subsonic Flutter Model Tests of Wings Carrying Heavy Tip Pods. Part 2. Swept Wings
Author(s): Brady, W. G., Maier, H. G., Pargoff, Walter T.Corporate Author(s): Cornell Aeronautical Laboratory, Inc.
Laboratory: Aircraft Laboratory
Date of Publication: 1954-11
Report number: WADC TR 53-161 Part 2
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A Study of Landing Gear Rebound and Subsequent Runout Characteristics
Author(s): Waterman, L. T., Sellers, W. H., Vickerym C. W., Kauffman, D. M.Corporate Author(s): Fairchild Engine and Airplace Corporation
Laboratory: Aircraft Laboratory
Date of Publication: 1954-03
Report number: WADC TR 54-110
full text available
The Effect of an Axially Symmetric Fuselage on the Nonstationary Supersonic Airloads Acting on a Wing with Supersonic Edges
Author(s): Epstein, MelvinCorporate Author(s): Aircraft Laboratory
Laboratory: Aircraft Laboratory
Date of Publication: 1954-05
Report number: WADC TR 54-196
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Flutter Characteristics of a T-Tail
Author(s): Pengelley, G. E., Wilson, L. E., Epperson, T. B., Ransleben, G. E.Corporate Author(s): Southwest Research Institute
Laboratory: Aircraft Laboratory
Date of Publication: 1954-11
Report number: WADC TR 52-162
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