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31 items
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Development Of Equipment For The Experimental Measurement Of The Moments Of Inertia, And Product Of Inertia Of Aircraft
Author(s): Woodward, Claude R.Corporate Author(s): Cornell Aeronautical Laboratory, Inc.
Laboratory: Aircraft Laboratory
Date of Publication: 1954-06
Report number: WADC TR 54-237
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The Effects Of Thermal Radiation On Aircraft Structures, Part 3. Structural Behavior Of Box-Beams Under Combined Static And Thermal Loads
Author(s): Loria, John C., Mar, James W., Engel, Seymour J.Corporate Author(s): Massachusetts Institute of Technology
Laboratory: Aircraft Laboratory
Date of Publication: 1957-06
Report number: WADC TR 54-384 Part 3
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Effects Of Structural Flexibility On Gust Loading Of Aircraft Part II: Dynamic Stresses In Swept-wing Airplanes
Author(s): Kirsch, A. A., Foss, K. A., Calligeros, J. M.Corporate Author(s): Peroelastic And Structures Research Laboratory, Massachusetts Institute Of Technology
Laboratory: Aircraft Laboratory
Date of Publication: 1955-08
Report number: WADC TR 54-592 Part 2
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Effects Of Structural Flexibility On Gust Loading Of Aircraft Part I: Gust Loads On Swept-wing Airplanes Free To Pitch And To Deform Statically
Author(s): Foss, K. A.Corporate Author(s): Peroelastic And Structures Research Laboratory, Massachusetts Institute Of Technology
Laboratory: Aircraft Laboratory
Date of Publication: 1955-03
Report number: WADC TR 54-592 Part 1
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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
full text available
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
full text available
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
full text available
Three-Dimensional Supersonic Flutter Model Tests Near Mach Number 1.5. Part II. Experimental And Theoretical Data For Bare wings And wings with Tip Tanks
Author(s): McCarthy, John F., Jr., Martuccelli, John R., Asher, Gifford W., Zartarian, GarabedCorporate Author(s): Massachusetts Institute of Technology
Laboratory: Aircraft Laboratory
Date of Publication: 1955-12
Report number: WADC TR 54-113 Part 2
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Three-dimensional Supersonic Flutter Model Tests Near Mach Number 1.5. Part 3: Experimental and Theoretical Data for Wings with Control Surfaces
Author(s): Asher, Gifford W., Weatherhill, Warren H.Corporate Author(s): Massachusetts Institute of Technology
Laboratory: Aircraft Laboratory
Date of Publication: 1958-01
Report number: WADC TR 54-113 Part 3
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Structural Design For Aerodynamic Heating. Part I: Design Information
Author(s): Dukes, W. H., Schnitt, A.Corporate Author(s): Bell Aircraft Corpoartion
Laboratory: Aircraft Laboratory
Date of Publication: 1955-10
Report number: WADC TR 55-305 Part 1
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