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31 items
![WADCTR54-196.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/a124394e9f4b368a781557db917ff53fa00bcc2e.jpg)
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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
![WADCTR55-179.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/50efd39250a7ebf0860053d76ff19cd417d97536.jpg)
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Coefficient of Friction of Aircraft Tires on Concrete Runways
Author(s): Luthman, Robert R.Corporate Author(s): University of Dayton
Laboratory: Aircraft Laboratory
Date of Publication: 1955-03
Report number: WADC TR 55-179
![WADCTR55-305part02.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/55bca6fe1a70eb1de717ebec64f81cb8b8f14f96.jpg)
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Structural Design for Aerodynamic Heating. Part II. Analytical Studies
Author(s): Dukes, W. H., Schnitt, A.Corporate Author(s): Bell Aircraft
Laboratory: Aircraft Laboratory
Date of Publication: 1955-10
Report number: WADC TR 55-305 Part 2
![WADCTR55-334.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/f1205c1f135274ad74e5842b23849f4a04bcbeed.jpg)
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Flutter Tests of Large Straight Wing Models at High Subsonic Speeds
Author(s): White, Richard P., Jr.Corporate Author(s): Cornell Aeronautical Laboratory, Inc.
Laboratory: Aircraft Laboratory
Date of Publication: 1955-12
Report number: WADC TR 55-334
![WADCTR55-259.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/f73a4dd2a0eabea7bcc0c45f0e1d56bdd488d9fd.jpg)
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Fabrication and Testing of Full Scale Polyester Canopies
Author(s): Harley, Robert E., Frownfelter, Charles R., Burkley, Ralph A.Corporate Author(s): Goodyear Aircraft Corporation
Laboratory: Aircraft Laboratory
Date of Publication: 1955-06
Report number: WADC TR 55-259
![WADCTR55-097.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/f4f73e70ffa9d6f05415aae8c51a84e330ca35e4.jpg)
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Soundproofing Materials and the Installation Thereof in Aircraft
Author(s): Grafman, A. J.Corporate Author(s): Frank Mayer Engineering Company
Laboratory: Aircraft Laboratory
Date of Publication: 1955-03
Report number: WADC TR 55-97
![WADCTR56-285.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/17cf1b1b1e7ae8a5e3f1a20bc5c42b9581443177.jpg)
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Flutter Model Tests Of A Swept-back, All-moving Horizontal Tail At Supersonic Speeds
Author(s): Asher, Gifford W.Corporate Author(s): Massachusetts Inst Of Tech Cambridge
Laboratory: Aircraft Laboratory
Date of Publication: 1957-11
Report number: WADC TR 56-285
![WADCTR57-392.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/0333b42a550adb543bfd84b488c19e6dcd064ccd.jpg)
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Transonic Flutter Characteristics Of A 45 Degree Swept Back All Movable Stabilizer
Author(s): D'Ewart, Benjamin B., Jr., Farrell, Robert F.Corporate Author(s): Bell Aerospace Co Buffalo Ny
Laboratory: Aircraft Laboratory
Date of Publication: 1958-05
Report number: WADC TR 57-392
![WADCTR55-192volume02.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/f2ede77252ed90363500839862ce2d803c34c0e1.jpg)
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Studies On Thermal Stresses For Aircraft Structures Exposed To Transient External Heating, Volume II. An Analytical Method For The Prediction Of Behavior Of A Sheet-Stringer Panel With A Uniformly Heated Surface
Author(s): Mahlmeister, J. E.Corporate Author(s): California U.
Laboratory: Aircraft Laboratory
Date of Publication: 1955-12
Report number: WADC TR 55-192 Volume 2
![WADCTR55-192volume01.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/1633a52e2a4e3181a8b9c82256ceac9d22fa7a73.jpg)
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Studies on Thermal Stresses for Aircraft Structures Exposed to Transient External Heating. Volume I. Evaluation of the Thermal Response, Force and Moment in a Plate.
Author(s): Mahlmeister, J. E., Ambrosio, A., Ishimoto, TCorporate Author(s): University of California, Los Angeles, Department of Engineering
Laboratory: Aircraft Laboratory
Date of Publication: 1955-04
Report number: WADC TR 55-192 Volume 1
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