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Research project

Sandham - Jet noise from in stability mode interactions

Staff

Lead researchers

Professor Neil Sandham

Professor of Aerospace Engineering

Research interests

  • Transonic aerodynamics of wings
  • Hypersonic flows with transition to turbulence
  • Flow over rough surfaces
Connect with Neil

Email: [email protected]

Other researchers

Dr Zhiwei Hu

Associate Professor
Connect with Zhiwei

Email: [email protected]

Collaborating research institutes, centres and groups

Research outputs

Transitional shock-wave/boundary-layer interactions in hypersonic flow
N.D. Sandham, E. Schuelein, A Wagner, S Willems & J Steelant, 2014, Journal of Fluid Mechanics, 752, 1-33
DOI: 10.1017/jfm.2014.333
Type: article
On the Mach number and temperature dependence of jet noise: Results from a simplified numerical model
V. Suponitsky, N. D. Sandham & Anurag Agarwal, 2011, Journal of Sound and Vibration, 330(17), 4123-4138
DOI: 10.1016/j.jsv.2011.02.007
Type: article
DNS of a canonical compressible nozzle flow
R.D. Sandberg, V. Suponitsky & N.D. Sandham, 2010
DOI: 10.1007/978-94-007-2482-2_46
Type: conference
Linear and nonlinear mechanisms of sound radiation by instability waves in subsonic jets
Victoria Suponitsky, Neil D. Sandham & Christopher L. Morfey, 2010, Journal of Fluid Mechanics, 658, 509-538
DOI: 10.1017/S0022112010002375
Type: article
Direct numerical simulation of the early development of a turbulent mixing layer downstream of a splitter plate
Neil D. Sandham & Richard D. Sandberg, 2009, Journal of Turbulence, 10(1), 1-17
DOI: 10.1080/14685240802698774
Type: article