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Low-lift drag and stability data from rocket models of a modified-delta-wing airplane with and without external stores at Mach numbers from 0.8 to 1.36

Grady L. Mitcham, Willard S. Blanchard

Abstract

Report presenting a flight investigation to determine the drag and stability at low lift coefficients of models of a modified-delta-wing airplane at a range of Mach and Reynolds numbers. A summary of the drag and stability data from the tests is provided.

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Available abstract

Key concepts: Airplane, Lift-to-drag ratio, Drag, Lift-induced drag, Mach number, Aerospace engineering, Lift (data mining), Longitudinal static stability