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Temp-Tapes: Improved Design, Construction, And Calibration
Author(s): Ambrosio, Alphonso, Busseli, Bertram
Corporate Author(s): University Of California, Department Of Engineering
Laboratory: Aircraft Laboratory
Date of Publication: 1953-07
Report number: WADC TR 53-211
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Temperature Distributions In A Typical Aircraft Structure Due To Transient External Heating, Volume I, T-33 Airplane
Author(s): Ambrosio, Alphonso, Bussell, Bertram, Macinnes, William F.
Corporate Author(s): University Of California, Department Of Engineering, Los Angeles, California
Laboratory: Aircraft Laboratory
Date of Publication: 1953-04
Report number: WADC TR 52-216
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Analytical Studies Of Aircraft Structures Exposed To Transient External Heating Volume III Thermal Response Of The Skin And Support Flange Of A Structural Joint
Author(s): Ambrosio, Alphonso, Ishimoto, Takao
Corporate Author(s): University 0f California, Department Of Engineering
Laboratory: Aircraft Laboratory
Date of Publication: 1955-01
Report number: WADC TR 54-579 Volume 3
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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, Takao
Corporate 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, Takao
Corporate 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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Thermal Response Of A Thin Plate With Radiation Losses
Author(s): Ambrosio, Alphonso, Ishimoto, Takao
Corporate Author(s): Dept. Of Engineering, University of California
Laboratory: Aircraft Laboratory
Date of Publication: 1958-06
Report number: WADC TR 56-212

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