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Transonic mach number sweep system for the NAL 4'x4' trisonic wind tunnel

KV Srikantan

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Abstract

This note describes the design of Transonic Mach Number Sweep system meant to vaxy the Mach number during a b1owdown in the Transonic range (M = 0.8 to 1.40). Mach number steps are achieved by preset controlled operation of Transonic Control13; Flaps. The stepwise increase in Mach number is obtained through divergence of the flaps and vice versa.

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What this paper is about

This note describes the design of Transonic Mach Number Sweep system meant to vaxy the Mach number during a b1owdown in the Transonic range (M = 0.8 to 1.40). Mach number steps are achieved by preset controlled operation of Transonic Control13; Flaps. The stepwise increase in Mach number is obtained through divergence of the flaps and vice versa.

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Available abstract

This note describes the design of Transonic Mach Number Sweep system meant to vaxy the Mach number during a b1owdown in the Transonic range (M = 0.8 to 1.40). Mach number steps are achieved by preset controlled operation of Transonic Control13; Flaps. The stepwise increase in Mach number is obtained through divergence of the flaps and vice versa.

Key concepts: Transonic, Mach number, Drag divergence Mach number, Subsonic and transonic wind tunnel, Aerospace engineering, Mathematics, Aerodynamics, Engineering

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Transonic mach number sweep system for the NAL 4'x4' trisonic wind tunnel — Research Paper | ScholarLens