Loughborough University
Leicestershire, UK
LE11 3TU
+44 (0)1509 263171
Loughborough University

Loughborough University Institutional Repository

Please use this identifier to cite or link to this item: https://dspace.lboro.ac.uk/2134/18101

Title: Underexpanded jet development from a rectangular nozzle with aft-deck
Authors: Behrouzi, P.
McGuirk, James J.
Issue Date: 2015
Publisher: © American Institute of Aeronautics and Astronautics
Citation: BEHROUZI, P. and MCGUIRK, J.J., 2015. Underexpanded jet development from a rectangular nozzle with aft-deck. AIAA Journal, 53 (5), pp. 1287 - 1298.
Abstract: An experimental study is reported of underexpanded supersonic jet plumes issuing from a high-aspect-ratio convergent rectangular nozzle. Schlieren visualization, Pitot probe, and Laser Doppler Anemometry measurements are carried out to capture the plume development in the near field, and in particular the effect on the plume flow of a finite-length extended shelf or aft-deck attached to the lower nozzle wall. This creates asymmetry in the inviscid shock cell pattern and the entrainment characteristics, both of which influence shear-layer growth and plume trajectory. A net pressure force is induced on the aft-deck wall, which leads to transverse deflection of the jet plume once it leaves the aft-deck, both upward and downward, depending on aft-deck length and nozzle pressure ratio. For sufficiently high nozzle pressure ratio and a sufficiently long aft-deck, separation and reattachment of the plume from the aft-deck is observed. Detailed mapping of both mean velocity and turbulence in the plume near field has been carried out, enabling comparison of flow behavior for a clean nozzle and a nozzle with aft-deck. The data provided are proposed as a suitable benchmark validation test case for computational fluid dynamics studies of rectangular nozzle plumes with aft-deck interaction effects.
Description: This is the accepted version of an article that was subsequently published in the AIAA Journal [© AIAA]. The definitive version is available at: http://dx.doi.org/10.2514/1.J053376
Version: Accepted for publication
DOI: 10.2514/1.J053376
URI: https://dspace.lboro.ac.uk/2134/18101
Publisher Link: http://dx.doi.org/10.2514/1.J053376
ISSN: 0001-1452
Appears in Collections:Published Articles (Aeronautical and Automotive Engineering)

Files associated with this item:

File Description SizeFormat
AIAA_Underexpanded_Jet_Rect_Nozzle_Aft-Deck_Final.pdfAccepted version1.87 MBAdobe PDFView/Open

 

SFX Query

Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.