John E Hatch, James Gallagher
Abstract
From Introduction: The purpose of this paper is to provide further information on the effects of Reynolds number on the aerodynamic characteristics of the wing of reference 1 as well as to provide load distributions for the wing at Mach numbers of 1.6 and 1.9.
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From Introduction: The purpose of this paper is to provide further information on the effects of Reynolds number on the aerodynamic characteristics of the wing of reference 1 as well as to provide load distributions for the wing at Mach numbers of 1.6 and 1.9.
Key concepts: Reynolds number, Mach number, Aerodynamics, Delta wing, Wing, Range (aeronautics), Mechanics, Mathematics