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15 - General Engineering

University of Cambridge

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Article title

Microramp control of supersonic oblique shock-wave/boundary-layer interactions

Type

D - Journal article

DOI

10.2514/1.38022

Title of journal

AIAA Journal

Article number

Volume number

Issue number

First page of article

668

ISSN of journal

0001-1452

Year of publication

2009

URL

http://www.aiaa.org/content.cfm?pageid=322&lupubid=2

Number of additional authors

Additional information

This paper demonstrated the potential of separation control with micro-vortex-generators which led to several research grants in supersonic inlet flow control. This includes funding from the US Air Force (EOARD ref FA8655, USD160k) and Lockheed Martin Inc. (USD130k, RG53319 and RG62670). Due to the demonstrated expertise, Cambridge are the only non-US participant at NASA's annual invited-only Supersonic Inlet Workshop (now in its 6th year) and Babinsky was asked to organise and co-chair two sessions on supersonic inlet aerodynamics at the 50th AIAA Aerospace Sciences Meeting in 2012. Subsequently developed vortex generator geometries are now patented under US Patent No.61/277878.

Interdisciplinary

Cross-referral requested

Research group

None

Proposed double-weighted

Double-weighted statement

Reserve for a double-weighted output

Non-English

English abstract