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Lift, drag and thrust measurement in a hypersonic impulse facility (1995)

Mee, D. J. ; Tuttle, S. L. ; Simmons, J. M.

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Publication Date: 2019-07-13

Description: This paper reports the extension of the stress wave force balance to the measurement of forces on models which are non-axisymmetric or which have non-axisymmetric load distributions. Recent results are presented which demonstrate the performance of the stress wave force balance for drag measurement, for three-component force measurement and preliminary results for thrust measurement on a two-dimensional scramjet nozzle. In all cases, the balances respond within a few hundred microseconds.

Keywords: AERODYNAMICS

Type: AIAA PAPER 94-2596 , AIAA Aerospace Ground Testing Conference; Jun 20, 1994 - Jun 23, 1994; Colorado Springs, CO; United States|Shock Tunnel Studies of Scramjet Phenomena 1994; 9 p

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