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12 items
![WADDTR60-773article16.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/513a64f4335d16a482fac64f1ca56403d114ff12.jpg)
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Anodic Coatings for Temperature Control in Space Vehicles
Author(s): Cooke, E. W., Long, W. L.Corporate Author(s): North American Aviation, Inc.
Laboratory: Materials Central
Date of Publication: 1961-07
Report number: WADD TR 60-773 p. 281-298
![FDLTDR64-043.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/726015376dc7c5c30c201ae3fb38200cc268114c.jpg)
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Confac II, A General Computer Program for the Determination of Radiant-Interchange Configuration and Form Factors
Author(s): Toups, Kempton A.Corporate Author(s): North American Aviation, Inc.
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1964-04
Report number: FDL TDR 64-43
![AFAPLTR65-108article22.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/e5a4bfb845d428b43380e73394ccea9148b3e919.jpg)
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Potential Applications for Expandable and Inflatable Structures for Re-entry Vehicles
Author(s): Wykes, R. P.Corporate Author(s): North American Aviation, Inc.
Laboratory: Air Force Aero Propulsion Laboratory
Date of Publication: 1965-05-27
Report number: AFAPL TR 65-108 p. 497-518
![AFAPLTR65-108article30.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/8fd486f91abd6cfaf3fc5379a176c6c69e87a721.jpg)
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Structural Behavior of Tapered Inflated Fabric Cylinders Under Various Loading Conditions
Author(s): Kovalesvsky, L., Rish, F. L.Corporate Author(s): North American Aviation, Inc.
Laboratory: Air Force Aero Propulsion Laboratory
Date of Publication: 1965-05-27
Report number: AFAPL TR 65-108 p. 659-685
![AFFDLTR65-090.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/0c6f2ca3a39f4500f6a946638e72dec466332eef.jpg)
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Self-Adaptive Flight Control by Multivariable Parameter Identification
Author(s): Shipley, P. P., Engel, A. G., Jr., Hung, J. W.Corporate Author(s): North American Aviation, Inc.
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1965-08
Report number: AFFDL TR 65-90
![AFFDLTR66-080article33.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/053d962072f070e31b6f5d73f5e1b8cf9bc77606.jpg)
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Matrix Error Analysis for Engineers
Author(s): Rosanoff, R. A., Ginsbur, T. A.Corporate Author(s): North American Aviation, Inc.
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1966-11
Report number: AFFDL-TR-66-80 p. 887-910
![AFFDLTR66-078.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/7a3a0c155048a15688f8092411f56b33ca955feb.jpg)
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Sonic Fatigue Tolerance of Glass Filament Structure: Experimental Results
Author(s): Hayes, J. A.Corporate Author(s): North American Aviation, Inc.
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1966-12
Report number: AFFDL TR 66-78
![AFFDLTR66-080article02.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/cb018488872911d1b71ec26d064886f52a0b974e.jpg)
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A Regularization Method for Calculation of Stresses, Deformations, and Elastic Modes
Author(s): Falconer, Robert W., Lane, Robert D.Corporate Author(s): North American Aviation, Inc.
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1966-11
Report number: AFFDL-TR-66-80 p. 191-204
![AFFDLTR66-080article09.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/f59df0c9372c1535fda34aa31b2b306c446ef9bb.jpg)
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Structural Influence Coefficients for a Redundant System Including Beam-Column Effects
Author(s): Rodden, William P.Corporate Author(s): North American Aviation, Inc.
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1966-11
Report number: AFFDL-TR-66-80 p. 353-383
![AFFDLTR65-171.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/17a29f3494c5f63f22a8531c3d354a32aa295baa.jpg)
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Modeling Techniques for Sonic Fatigue Prediction
Author(s): Wang, P.Corporate Author(s): North American Aviation, Inc.
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1966-06
Report number: AFFDL TR 65-171
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