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Hypersonic free-flight dynamic stability studies

Hypersonic free-flight dynamic stability studies
Hypersonic free-flight dynamic stability studies

This work discusses the development of and subsequent use of a novel method for the measurement of stability derivatives of models in a hypersonic gun tunnel using the free-flight technique. The technique uses a passive electro-optical system to illuminate and scan a rectangular field of view in the vertical plane through the test-section of the gun tunnel. 6 vertical laser sheets, produced by the expansion and reflection of 3 He-Ne laser sources, are used to backlight the model as it flies through the field of view. Shadows from sheets interrupted by the model are projected onto rapid-access photo-sensitive arrays. The position and pitch angle of a model traversing the field of view can be determined by a knowledge of the recorded shadow positions and the external geometry.

The non-linear differential equations of motion are fitted to the resulting motions using a parametric differentiation technique embedded in a modified least-squares minimisation scheme. Convergence of the minimisation procedure yields the stability terms which are of interest.

The effects of model geometry and mass distribution on the resulting free-flight static and dynamic stability are assessed and discussed.

University of Southampton
Lewis, Harvey Owen
Lewis, Harvey Owen

Lewis, Harvey Owen (1996) Hypersonic free-flight dynamic stability studies. University of Southampton, Doctoral Thesis.

Record type: Thesis (Doctoral)

Abstract

This work discusses the development of and subsequent use of a novel method for the measurement of stability derivatives of models in a hypersonic gun tunnel using the free-flight technique. The technique uses a passive electro-optical system to illuminate and scan a rectangular field of view in the vertical plane through the test-section of the gun tunnel. 6 vertical laser sheets, produced by the expansion and reflection of 3 He-Ne laser sources, are used to backlight the model as it flies through the field of view. Shadows from sheets interrupted by the model are projected onto rapid-access photo-sensitive arrays. The position and pitch angle of a model traversing the field of view can be determined by a knowledge of the recorded shadow positions and the external geometry.

The non-linear differential equations of motion are fitted to the resulting motions using a parametric differentiation technique embedded in a modified least-squares minimisation scheme. Convergence of the minimisation procedure yields the stability terms which are of interest.

The effects of model geometry and mass distribution on the resulting free-flight static and dynamic stability are assessed and discussed.

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More information

Published date: 1996

Identifiers

Local EPrints ID: 459660
URI: http://eprints.soton.ac.uk/id/eprint/459660
PURE UUID: 66c64147-2cd7-49d0-9a87-00c6180f4306

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Date deposited: 04 Jul 2022 17:16
Last modified: 04 Jul 2022 17:16

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Contributors

Author: Harvey Owen Lewis

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