Preliminary Evaluation of Flight-Weight XRJ47-W-5 Ram-Jet Engine at a Mach Number of 2.75
Description:
Report presenting a free-jet investigation of the performance, burner-shell cooling, and ignition characteristics of a flight-weight 48-inch-diameter XRJ47-W-5 ramjet engine at an inlet Mach number of 2.75 and an angle of attack of 3 degrees. Data were obtained over a range of altitudes, inlet temperatures, and fuel-air ratios.
Date:
July 26, 1955
Creator:
Welna, Harry J. & Reilly, Dwight H.
Item Type:
Refine your search to only
Report
Partner:
UNT Libraries Government Documents Department