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Tabulated pressure coefficients and aerodynamic characteristics measured on the wing of the Bell X-1 airplane in pull-ups at Mach numbers from 0.53 to 0.99

Ronald J. Knapp, Gertrude V. Wilken

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Abstract

Tabulated pressure coefficients and aerodynamic characteristics are presented for six spanwise stations on the left wing of the Bell X-1 research airplane. The data were obtained in 10 pull-ups at Mach numbers from 0.53 to 0.99 (p. 1).

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What this paper is about

Tabulated pressure coefficients and aerodynamic characteristics are presented for six spanwise stations on the left wing of the Bell X-1 research airplane. The data were obtained in 10 pull-ups at Mach numbers from 0.53 to 0.99 (p. 1).

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Available abstract

Tabulated pressure coefficients and aerodynamic characteristics are presented for six spanwise stations on the left wing of the Bell X-1 research airplane. The data were obtained in 10 pull-ups at Mach numbers from 0.53 to 0.99 (p. 1).

Key concepts: Mach number, Airplane, Aerodynamics, Wing, Dynamic pressure, Wing loading, Aerospace engineering, Aeronautics

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Tabulated pressure coefficients and aerodynamic characteristics measured on the wing of the Bell X-1 airplane in pull-ups at Mach numbers from 0.53 to 0.99 — Research Paper | ScholarLens