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41 items
![AEDCTDR62-218.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/1c509327e81d911f695e05a8f946cdb9f3b95bf8.jpg)
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Measurements of Pressure and Speed of Flow in a Spark-Heated Hypersonic Wind Tunnel
Author(s): Karamcheti, Krishnamurty, Vali, Walter, Kyser, James B., Rasmussen, Maurice L.Corporate Author(s): Stanford University
Laboratory: Arnold Engineering Development Center
Date of Publication: 1962-11
Report number: AEDC TDR 62-218
![AEDCTDR62-213.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/aa7b1a6053d0aa36aa600b4be10ddec2cb8a7ac5.jpg)
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Microwave Measurement of Projectile Kinematics Within Launcher Barrels
Author(s): Hendrix, R. E.Corporate Author(s): ARO, Inc.
Laboratory: Arnold Engineering Development Center
Date of Publication: 1962-11
Report number: AEDC TDR 62-213
![AEDCTDR62-221.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/008ae87b7ea02c687fca466b090e429f095caa76.jpg)
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Evaluation of a Gas Bearing Pivot for a High Amplitude Dynamic Stability Balance
Author(s): Hodapp, A. E., Jr.Corporate Author(s): ARO, Inc.
Laboratory: Arnold Engineering Development Center
Date of Publication: 1962-12
Report number: AEDC TDR 62-221
full text by request
Inviscid and Viscous Hypersonic Nozzle Flow with Finite Rate Chemical Reactions
Author(s): Levinsky, E. S., Brainerd, J. J.Corporate Author(s): General Dynamics/Astronautics
Laboratory: Arnold Engineering Development Center
Date of Publication: 1963-01
Report number: AEDC TDR 63-18
![AEDCTDR63-137.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/acce4b303ff999db59b5653cdd0d7927b70d5b7c.jpg)
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Force Tests of Standard Hypervelocity Ballistic Models HB-1 and HB-2 at Mach 1.5 to 10
Author(s): Gray, J. Don, Lindsay, E. EarlCorporate Author(s): ARO, Inc.
Laboratory: Arnold Engineering Development Center
Date of Publication: 1963-08
Report number: AEDC TDR 63-137
full text unavailable
Methods of Approximating Inviscid Jet Boundaries for Highly Underexpanded Supersonic Nozzles
Author(s): Henson, J. R., Robertson, J. E.Corporate Author(s): Arnold Engineering Development Center
Laboratory: Arnold Engineering Development Center
Date of Publication: 1962-05
Report number: AEDC TDR 62-7
full text unavailable
Development of a Gas Generator Using a Rocket-Type Combustor as the Heat Source
Author(s): Carman, C. T.Corporate Author(s): Arnold Engineering Development Center
Laboratory: Arnold Engineering Development Center
Date of Publication: 1962-03
Report number: AEDC TDR 62-15
full text unavailable
Flow-Field Investigation of a 0.0667-Scale Model of the X-15 Research Vehicle at Mach 4, 6, 8
Author(s): Rippey, J.Corporate Author(s): ARO, inc.
Laboratory: Arnold Engineering Development Center
Date of Publication: 1964-10
Report number: AEDC -TDR-201
![AEDCTR80-011.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/cba3c287dbe48eccf17614354e933ac75757bb93.jpg)
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Missile Motion Sensitivity to Dynamic Stability Derivatives
Author(s): Langham, T. F.Corporate Author(s): ARO, Inc.
Laboratory: Arnold Engineering Development Center
Date of Publication: 1980-09-01
Report number: AEDC TR 80-11
full text by request
Numerical Solution of the Three-Dimensional Unsteady Euler Equations
Author(s): Koeing, K., Barton, J. M.Corporate Author(s): Mississippi State University; Sverdrup Technology, Inc.
Laboratory: Arnold Engineering Development Center
Date of Publication: 1983-08-01
Report number: AEDC TR 83-22
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