Flight Investigation of a Roll-Stabilized Ramjet Test Vehicle over a Mach Number Range of 2.3 to 2.7, 7 October 1955

Flight Investigation of a Roll-Stabilized Ramjet Test Vehicle over a Mach Number Range of 2.3 to 2.7, 7 October 1955

Background

A flight investigation has been conducted on a roll-stabilized ramjet test vehicle. Engine performance data are presented over a Mach number range of 2.3 to 2.7, a range of fuel-air ratio of 0.038 to 0.050, and an altitude range of 3,000 to 40,000 feet. Roll-control performance is presented over a Mach number range of approximately 2.3 to 2.4. Theoretical values of the half amplitude and the period of the self sustained roll oscillation show good agreement with experimental results.

Document Archive

 Flight Investigation of a Roll-Stabilized Ramjet Test Vehicle over a Mach Number Range of 2.3 to 2.7, 7 October 1955 [30 Pages, 9.6MB]

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