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33 items
![AFFDLTR64-187.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/1f385d0799f814675bce663d44d1a42bdc58b218.jpg)
full text available
The Effects of Active Cooling on the Aerodynamic and Aerothermodynamic Characteristics of Slender Bodies of Revolution
Author(s): Leadon, B. M., Rosciszeski, Jan., Gallaher, W. H., Holst, W. R., Carter, W. V.Corporate Author(s): General Dynamics/Convair
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-12
Report number: AFFDL TR 64-187
full text by request
The Effect of Surface Perturbations on the Pressure Distributions About Blunt Two-Dimensional Bodies at High Mach Numbers
Author(s): Donaldson, Coleman duP., Sullivan, Roger D., Hayes, Wallace D.Corporate Author(s): Aeronautical Research Associates of Princeton, Inc.
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-04
Report number: FDL TDR 64-17
![FDLTDR64-026.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/abe856ff65407c49cd03c83a80066f8cc120e579.jpg)
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Analytical and Experimental Investigation of the Acoustic Environment of the RTD Sonic Fatigue Main Test Chamber
Author(s): Tyzzer, Franklin G., Pernet, David F.Corporate Author(s): IIT Research Institute
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-04
Report number: FDL TDR 64-26
![FDLTDR64-042.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/30e916a680014effb7ae8a2c50a6f5f69c341eb9.jpg)
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Measurement of Angular Displacements of Practical Wing Structures by the Moire' Fringe Technique
Author(s): Padlog, Joseph, Gallagher, Richard H.Corporate Author(s): Bell Aerosystems Company
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-09
Report number: FDL TDR 64-42
![FDLTDR64-048part01.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/491e3511a0c83735cf935842ce1fa51eea3c19a6.jpg)
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Control Systems Theory Applied to the Re-Entry of Aerospace Vehicles - II
Author(s): Kishi, F. H.Corporate Author(s): University of California
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-08
Report number: FDL TDR 64-48 Part 1
![FDLTDR64-049part01.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/9c859b7376c42a1462987631e2eb655d46ebfda0.jpg)
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Model Fly Program, Part I. Theoretical Investigations and Preliminary Design Considerations
Author(s): Hill, J. A., Gikas, X. A., Fonda, A. G., Gargani, A. J.Corporate Author(s): Giannini Controls Corporation
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-07
Report number: FDL TDR 64-49 Part 1
![FDLTDR64-060.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/0fdcaead28edab50cb5ff0b1b081d126ec25bdae.jpg)
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Flight Evaluation of Various Short Period Dynamics at Four Drag Configurations for the Landing Approach Task
Author(s): Chalk, Charles R.Corporate Author(s): Cornell Aeronautical Laboratory
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-10
Report number: FDL TDR 64-60
![FDLTDR64-067part01.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/c9f3803a0ec14d0c46821eb55bfcf7bf2d7fb6aa.jpg)
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Carbon Monoxide Management, Part I: Technique for Carbon Dioxide Absorber Evaluation
Author(s): Allen, John P.Corporate Author(s): AF Air Flight Dynamics Laboratory
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-06
Report number: FDL TDR 64-67 Part 1
![FDLTDR64-120.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/e2f97563261c3377ff91085a130db63b7ebd0077.jpg)
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Pressure and Heat Transfer Measurements fro Mach 21 Flows Over a Blunt Pyramidal Configuration with Aerodynamic Controls
Author(s): Kaufman, Louis G., IICorporate Author(s): Grumman Aircraft Engineering Corporation
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-08
Report number: FDL TDR 64-120
![FDLTDR64-142.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/c2d9448d1bacdaaff536bdccde11aec4552b4694.jpg)
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Heat Transfer Measurements at Mach 9 on an Aerodynamically Controllable Winged Re-Entry Configuration: Part of an Investigation of Hypersonic Flow Separation and Control Characteristics
Author(s): Meckler, LawrenceCorporate Author(s): Grumman Aircraft Engineering Corporation
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-09
Report number: FDL TDR 64-142
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