Title: Preliminary Flight Measurements of the Total Pressure Recovery of a Split-Wing RAM-Jet Inlet at Mach Numbers from 1.4 to 3.16
Abstract: From Summary: Flight tests were made to determine the total-pressure recovery of a split-wing ram-jet inlet with a fixed area exit 20 percent larger than the inlet throat over a Mach number range from 1.4 to 3.16. Total-pressure-recovery measurements at the diffuser exist station indicated abrupt pressure changes in the total-pressure profile throughout the Mach number range. Comparisons of average total-pressure recovery with the theoretical total-pressure recovery showed good agreement.
Publication Year: 2013
Publication Date: 2013-07-31
Language: en
Type: book
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