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41 items
![AEDCTDR62-137.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/038c1e68cb4d83a5b4fccfecf3ab0ff503f0ea3c.jpg)
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Inductive Power Supply For A Hotshot-Type Tunnel
Author(s): Fillers, A. H., Jr.Corporate Author(s): Arnold Engineering Development Center Arnold Air Force Station Tenn
Laboratory: Arnold Engineering Development Center
Date of Publication: 1962-07
Report number: AEDC TDR 62-137
![AEDCTDR62-141.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/b5a1f93d8844a1b16ccbcf52e820bba2edc54502.jpg)
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Radio Telemetry of Stagnation Pressure from a wind Tunnel Model Magnetically Supported in Supersonic Flow,
Author(s): Clemens, P. L.Corporate Author(s): Arnold Engineering Development Center Arnold Air Force Station Tenn
Laboratory: Arnold Engineering Development Center
Date of Publication: 1962-07
Report number: AEDC TDR 62-141
![AEDCTDR62-155.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/b92cecb40f126115d9e46b02d79f3b4509f5d0a3.jpg)
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Experimental Heat Transfer to Blunt Axisymmetric Bodies Near the Limit of Continuum Flow
Author(s): Potter, J. Leith, Miller, John T.Corporate Author(s): ARO, Inc.
Laboratory: Arnold Engineering Development Center
Date of Publication: 1962-08
Report number: AEDC TDR 62-155
![AEDCTDR62-168.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/d45b26aaacba650f672df0c442affd16849b30ba.jpg)
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Fatigue Tests and Crack Detection on Some Types of Axial-Flow Compressor Rotor Blades
Author(s): Thomas, R. E.Corporate Author(s): ARO, Inc.
Laboratory: Arnold Engineering Development Center
Date of Publication: 1962-10
Report number: AEDC TDR 62-168
![AEDCTDR62-170.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/ba76b964f04c9af7597ad378f1a41c853d64c8ff.jpg)
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Tables of the Thermodynamic Properties of Nitrogen From 100 to 1500°K
Author(s): Little, Wanda J., Neel, C. A.Corporate Author(s): ARO, Inc.
Laboratory: Arnold Engineering Development Center
Date of Publication: 1962-09
Report number: AEDC TDR 62-170
![AEDCTDR62-172.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/1084ce721c577890ccc191125aa5ab8d9d95bfbd.jpg)
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An Analysis of Nonequilibrium Inviscid Flow
Author(s): Gibson, W. E., Sowydra, A.Corporate Author(s): Cornell Aeronautical, Inc.
Laboratory: Arnold Engineering Development Center
Date of Publication: 1962-08
Report number: AEDC TDR 62-172
![AEDCTDR62-174.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/c6de66053db82f7afbe233d7c3848ab2dc7b891d.jpg)
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A Two-Color Pyrometer for the Measurement of Temperature and Contamination Level in a Spark-Heated Hypervelocity Wind Tunnel
Author(s): Vali, Walter, de Voto, R. StephenCorporate Author(s): Stanford University
Laboratory: Arnold Engineering Development Center
Date of Publication: 1962-08
Report number: AEDC TDR 62-174
![AEDCTDR62-188.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/ae491e610e2183eec10d7775e560f624fb2e457a.jpg)
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Addendum to an Investigation of the Equilibrium Pressure Along Unequally Heated Tubes
Author(s): Bailey, A. B., Arney, G. D., Jr.Corporate Author(s): ARO, Inc.
Laboratory: Arnold Engineering Development Center
Date of Publication: 1962-10
Report number: AEDC TDR 62-188
![AEDCTDR62-205.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/47a87c1e6c8b425f98ddae24145928e6392096fc.jpg)
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The Drag of Spheres in Rarefied Hypervelocity Flow
Author(s): Kinslow, Max, Potter, J. L.Corporate Author(s): ARO, Inc.
Laboratory: Arnold Engineering Development Center
Date of Publication: 1962-12
Report number: AEDC TDR 62-205
![AEDCTDR62-208.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/64aef46f6981b93b62e535faed559891a34d3280.jpg)
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Further Experiments on Impact-Pressure Probes in a Low-Density, Hypervelocity Flow
Author(s): Bailey, A. B.Corporate Author(s): ARO, Inc.
Laboratory: Arnold Engineering Development Center
Date of Publication: 1962-11
Report number: AEDC TDR 62-208
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