Highly Influential Citations1
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Abstract : The flow about a slender flat-plate delta wing at angle of-attack is represented by replacing the vortex core-feeding sheet system associated with leading edge separation by a force-free… Continue Reading
A simple procedure was developed for the estimation of road vehicle aerodynamic drag based on easily quantifiable vehicle shape parameters. The procedure is applicable to passenger vehicles, station… Continue Reading
Abstract : A set of hypersonic aerodynamic characteristics has been obtained for the Gemini re-entry module by a least squares curve fit of the appropriate ground test data to equation forms which… Continue Reading
An engineering model for the supersonic portion of the turbulent near wake behind a re-entry vehicle is presented. By treating only the supersonic regions, the saddle-point singularities present in… Continue Reading