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Development of a subscale supersonic aeropropulsion wind tunnel

descriptionPublicationkeyboard_double_arrow_right Article , Other literature type 15 Jun 1998Publisher:American Institute of Aeronautics and Astronautics (AIAA)Journal:20th AIAA Advanced Measurement and Ground Testing Technology Conference

Authors: Donald R. Wilson; Frank K. Lu; George Matsumoto;

doi: 10.2514/6.1998-2868

Development of a subscale supersonic aeropropulsion wind tunnel

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Abstract

The preliminary design of a Mach 1.5-4 blowdown wind tunnel is presented. The paper concentrates on the design of each of the tunnel components and also highlights the use of the tunnel for the study of the unsteadiness of the flow in the inlet and diffuser of pulse detonation engines. The design of the facility is almost completed and fabrication and assembly have started.

Related Organizations

The University of Texas at Arlington
United States

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	citations This is an alternative to the "Influence" indicator, which also reflects the overall/total impact of an article in the research community at large, based on the underlying citation network (diachronically).	4
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	impulse This indicator reflects the initial momentum of an article directly after its publication, based on the underlying citation network.	Average