Wind-Tunnel Investigation at Transonic Speeds of a Jet Control on an 80 Degree Delta-Wing Missile
Description:
Report presenting an investigation in the high speed tunnel of three missile models with cruciform delta wings swept back 80 degrees and equipped with jet controls to determine the effectiveness of the controls when using ram or mechanically compressed air. Results regarding the rolling characteristics, static rolling-moment coefficients, static pressure, and effect of the location of the jet control are provided.
Date:
November 1, 1955
Creator:
Turner, Thomas R. & Vogler, Raymond D.
Item Type:
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