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Correlation of low speed wind tunnel and flight test data for V/STOL aircraft

Woodrow L Cook, D. H. Hickey

Abstract

The XV-5B fan-in-wing aircraft and the Y0V-10 RCF rotating cylinder flap aircraft were subjected to wind tunnel tests. These tests were conducted specifically to provide for correlation between wind tunnel and inflight aerodynamics and noise test data. Correlation between aerodynamic and noise data are presented and testing techniques that are related to the accuracy of the data, or that might affect the correlations, are discussed.

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Available abstract

Key concepts: Wind tunnel, Aerodynamics, Noise (video), Flight test, Aerospace engineering, Turboprop, Test data, Marine engineering