Expansion Tube Test Time Predictions

By: Nasa, National Aeronautics and Space Adm

The interaction of an interface between two gases and strong expansion is investigated and the effect on flow in an expansion tube is examined. Two mechanisms for the unsteady Pitot-pressure fluctuations found in the test section of an expansion tube are proposed. The first mechanism depends on the Rayleigh-Taylor instability of the driver-test gas interface in the presence of a strong expansion. The second mechanism depends on the reflection of the strong expansion from the interface. Predictions compare favorably with experimental results. The theory is expected to be independent of the absolute values of the initial expansion tube filling pressures. Gourlay, Christopher M. Unspecified Center EXPANSION; PREDICTIONS; SHOCK TESTS; SHOCK TUBES; TIME; HYPERVELOCITY; INTERFACES; SHOCK TUNNELS; STABILITY...

• Format: Paperback
• Language: English
• ISBN: 1730998739
• ISBN13: 9781730998737
• Release Date: January 1
• Publisher: Independently Published
• Length: 104 Pages
• Weight: 0.58 lbs.
• Dimensions: 0.2" x 8.5" x 11.0"