Lewis, Harvey Owen (1996) Hypersonic free-flight dynamic stability studies. University of Southampton, Doctoral Thesis.
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.
This record has no associated files available for download.
More information
Identifiers
Catalogue record
Export record
Contributors
Download statistics
Downloads from ePrints over the past year. Other digital versions may also be available to download e.g. from the publisher's website.