Read The Application of the Relief Technique for Velocity Field Measurements in the Astf C1 Test Cell - National Aeronautics and Space Administration file in ePub Online

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The Aeropropulsion Systems Test Facility (ASTF) C1 Test Cell is to be configured for propulsion tests of National Aerospace Plane (NASP) engines over flight Mach number conditions ranging from 0.5 to 3.8. This facility is capable of continuously generating a 5 ft. x 5 ft. square free air jet flow field at a local Mach number up to 3.32 with a density of between 0.134 and

Title : The Application of the Relief Technique for Velocity Field Measurements in the Astf C1 Test Cell
Author : National Aeronautics and Space Administration
Language : en
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Type : PDF, ePub, Kindle
Uploaded : Apr 07, 2021

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