eprintid: 11
rev_number: 4
eprint_status: archive
userid: 4
dir: disk0/00/00/00/11
datestamp: 2004-06-10
lastmod: 2015-05-29 19:45:19
status_changed: 2009-04-08 16:51:54
type: report
metadata_visibility: show
item_issues_count: 0
creators_name: Dellar, P.
creators_name: Howell, P.D.
contributors_name: Dewynne, J.
contributors_name: Edwards, C.M.
contributors_name: Fitt, A.D.
contributors_name: Kaouri, K.
contributors_name: Ockendon, H.
contributors_name: Ockendon, J.R.
contributors_name: Please, C.P.
contributors_name: Salazar-Gonzales, D.
title: Shock-free Supersonic Transport
ispublished: pub
subjects: aerodef
studygroups: esgi40
companyname: Vehicle Research Corporation
full_text_status: public
problem_statement: Vehicle Research Corporation has proposed a mechanism for eliminating the sonic boom generated by supersonic flight. It involves a nozzle-shaped wing underside, together with an underwing planar jet of engine compressor air. The Study Group was asked to provide a critical review of the proposed mechanism and a quantitative analysis of its likely performance.
date: 2001-04
date_type: published
pages: 11
citation:   Dellar, P. and Howell, P.D.  (2001) Shock-free Supersonic Transport.  [Study Group Report]     
document_url: http://miis.maths.ox.ac.uk/miis/11/1/ShockFree.pdf