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20 items
![AFFDLTR66-153part01.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/456f77a8a368ca9f03311b8b561d29dfa7766905.jpg)
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The Development And Evaluation Of The Cal/Air Force Dynamic Wind-Tunnel Testing System. Part I. Description And Dynamic Tests Of An F-80 Model
Author(s): Statler, Irving C., Tufts, Orren B., Hirtreiter, Walter J.Corporate Author(s): Cornell Aeronautical Lab Inc Buffalo N Y
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1967-02
Report number: AFFDL TR 66-153 Part 1
![AFFDLTR66-153part02.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/d9dce50ac1119574beeb8d2d20f1e17aca256af0.jpg)
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The Development And Evaluation Of The Cal/Air Force Dynamic Wind-Tunnel Testing System. Part II. Dynamic Tests Of An F-104 Model.
Author(s): Statler, Irving C.Corporate Author(s): Cornell Aeronautical Lab Inc Buffalo N Y
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1967-02
Report number: AFFDL TR 66-153 Part 2
![AFFDLTR66-170.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/a775db361acb7635f63f6abaaec30431540e5a40.jpg)
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Low Pressure Type Expandable Aircraft Tire Characteristics
Author(s): Wagner, Paul M.Corporate Author(s): Air Force Flight Dynamics Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1967-03
Report number: AFFDL TR 66-170
![AFFDLTR66-230.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/25da382a9004ccb29d770d072f7b752f5d8477f2.jpg)
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Investigation Of Ablation Effects On Hypersonic Dynamic Stability Of A 10 Deg. Cone.
Author(s): Moore, Dave R., Stalmach, Charles J., Jr., Pope, Thomas C.Corporate Author(s): LTV Aerospace Corp Dallas Tex LTV Vought Aeronautics Div
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1967-01
Report number: AFFDL TR 66-230
![AFFDLTR66-005.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/a331dcc48b27f2833a0f759c9fe89db9f4fa3afa.jpg)
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Preliminary Development of a Solid-State Matrix Display
Author(s): Lechner, B. J.Corporate Author(s): Radio Corporation of America
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1967-01
Report number: AFFDL TR 66-5
![FDLTDR64-149part02.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/a03fa650cb730974c215be45ce8fc18aaa4e9eab.jpg)
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Hypersonic Dynamic Stability: Part II. Conical Body Experimental Program
Author(s): Hobbs, R. B., Jr.Corporate Author(s): General Electric Company
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1967-01
Report number: FDL TDR 64-149 Part 2
![FDLTDR64-149part03.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/512835e133730ec8b1e1cadd5b6a9b88bfe6fa58.jpg)
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Hypersonic Dynamic Stability: Part III. Unsteady Flow Field Program
Author(s): Rie, H., Linkiewicz, E. A., Bosworth, F. D.Corporate Author(s): General Electric Company
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1967-01
Report number: FDL TDR 64-149 Part 3
![AFFDLTR67-144volume01.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/264813d3774d39e3e167b24cc8e5354f6966c675.jpg)
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Investigation of Turbulent Heat Transfer at Hypersonic Speeds. Volume I. Analytical Methods.
Author(s): Savage, Richard T., Jaeck, Carl L.Corporate Author(s): Boeing Company Aerospace Group, Seattle, Washington
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1967-12
Report number: AFFDL TR 67-144 Volume 1
![AFFDLTR67-119.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/cfd6563dd5df724a1fd62ad3d644a48c4b408304.jpg)
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Development And Experimental Evaluation Of A Retrieval System For Air Force Control-Display Information.
Author(s): Debons, Anthony, Scheffler, Frederic L., Snide, John D.Corporate Author(s): Dayton Univ Ohio Research Inst
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1967-11
Report number: AFFDL TR 67-119
![AFFDLTR67-010.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/92ee19ad881fdd5098827d10d11e7f9b83bc7022.jpg)
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Basis Of A Well Conditioned Force Program For Equilibrium Models Via The Southwell Slab Analogies
Author(s): de Veubeke, Baudouin M. FraeijsCorporate Author(s): Liege Univ (Belgium) Laboratoire D'aeronautique
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1967-03
Report number: AFFDL TR 67-10
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