This is a NACA test of a 20-inch diameter ramjet in the Altitude Wind Tunnel (AWT) on February 7, 1946.

The AWT analyzed the overall performance of ramjets at altitudes up to 47,000 feet. In this test, the ramjet was tested at altitudes ranging from 7000 to 41,500 feet and at ram-pressure ratios equivalent to free-stream Mach numbers as great as 1.84 using preheated 62-octane fuel.
From the report summary:
At an equivalent free-stream Mach number of 1.84 and a gas total-temperature ratio across the engine of 5.7, the equivalent sea-level net thrust was 8135 pounds. For these conditions, the over-all efficiency was 12.6 percent and the combustion efficiency was 70.3 percent. The corresponding net-thrust coefficient was 0.74. The investigation also showed that no change in the performance or operating range of the engine occurred when the fuel was changed from preheated 62-octane to preheated 100-octane gasoline.
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