The 1-MW Radiatively Driven Hypersonic Wind Tunnel Experiments

The 1-MW Radiatively Driven Hypersonic Wind Tunnel Experiments PDF Author:
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Languages : en
Pages : 134

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Results and analysis of the RDHWT/MARlAH II 1 MW experiment are reported. The experiment is the addition of approximately MW of energy to a supersonic air flow with an electron bean. The experiment hardware, arrangement and conduct are described. Selected data and analysis are reported. The experiment was subject to transient power fluctuations flat were traced to the electron beam source rather than to flow instability. Power stability was established at lower power conditions. and these data were used for selected code validations.

A 1 MW Radiatively-driven Hypersonic Wind Tunnel Experiment

A 1 MW Radiatively-driven Hypersonic Wind Tunnel Experiment PDF Author: Dennis K. Mansfield
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Languages : en
Pages :

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Fluid Mechanics in a Radiatively Driven Hypersonic Wind Tunnel

Fluid Mechanics in a Radiatively Driven Hypersonic Wind Tunnel PDF Author: G. L. Brown
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Languages : en
Pages :

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Radiatively Driven Hypersonic Wind Tunnel

Radiatively Driven Hypersonic Wind Tunnel PDF Author: R. Miles
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Languages : en
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One Dimensional Modeling of a Radiatively Driven Hypersonic Wind Tunnel

One Dimensional Modeling of a Radiatively Driven Hypersonic Wind Tunnel PDF Author: George Jarvis Williams
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Category :
Languages : en
Pages : 157

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Performance Characterization of a Radiatively Driven Hypersonic Wind Tunnel

Performance Characterization of a Radiatively Driven Hypersonic Wind Tunnel PDF Author: R. W. Anderson
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Languages : en
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Numerical Simulation and Design of a Radiatively Driven Hypersonic Wind Tunnel

Numerical Simulation and Design of a Radiatively Driven Hypersonic Wind Tunnel PDF Author: Robert W. Anderson
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Category :
Languages : en
Pages : 360

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Radiatively Driven Hypersonic Wind Tunnel

Radiatively Driven Hypersonic Wind Tunnel PDF Author:
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Category :
Languages : en
Pages : 0

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Work conduced from August 1, 1992 until November 30,1996 under support from the Air Force Arnold Engineering Development Center (AEDC), followed by continuing support from the Air Force Research Laboratory through September 30,1998, established the foundation for the development of a new concept which is expected to extend the range of practical hypersonic wind tunnel testing from approximately Mach 8 to Mach 12 and beyond.

Energy Addition and Thermalization Issues in a Radiatively-driven Hypersonic Wind Tunnel

Energy Addition and Thermalization Issues in a Radiatively-driven Hypersonic Wind Tunnel PDF Author: S. Macheret
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Languages : en
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Predictions for the Heat Transfer and Boundary Layer Growth in the Radiatively Driven Hypersonic Wind Tunnel and Camparisons with Experiment at Ultra High Reynolds Number (invited)

Predictions for the Heat Transfer and Boundary Layer Growth in the Radiatively Driven Hypersonic Wind Tunnel and Camparisons with Experiment at Ultra High Reynolds Number (invited) PDF Author: G. L. Brown
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Languages : en
Pages :

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