Shocks and Compressible Flows

Single-pixel PIV measurements of a differential-throttled aerospike nozzle jet in supersonic outer flow

P. Wißmann, C.J. Kähler, S. Scharnowski

Institute of Fluid Mechanics and Aerodynamics, University of the Bundeswehr Munich, 85577 Neubiberg, Germany

Non-Intrusive Measurements of Temperature and Velocity on a Sharp Cone at Mach 8

S.J. Beresh, W.C.B. Senior, D.R. Richardson

Sandia National Laboratories, Albuquerque, NM, 87185, USA

High-resolution velocity field in the first Mach disk region of an overexpanded supersonic jet

R. Jalain, S. Petit, B. Blaisot, N. Lupoglazoff, A. Langenais

ONERA/DMPE, Université Paris Saclay, F-91123, Palaiseau, France

Shock wave visualization in a 3D-printed axisymmetric critical flow venturi nozzle using Background-oriented Schlieren technique

M. Yamagishi, N. Takegawa, T. Morioka

National Metrology Institute of Japan (NMIJ), Advanced Institute of Science and Technology (AIST), Japan

High-Speed PIV Measurements of Transonic Shock-Buffet Control on a Supercritical Airfoil with Air-Jet Vortex Generators

D.P. Ramaswamy, S. Scharnowski, C.J. Kähler

Institute of Fluid Mechanics and Aerodynamics, University of the Bundeswehr Munich, 85577 Neubiberg, Germany

Fast Pressure-Sensitive Paint Imaging Of Three-Dimensional Non-Stationary Shock Oscillations In A Mach-5 Intake With Synchronised Schlieren Support

M.T. Gurbuz(1), E.J. Nunn(2), O. Ozer(3), K.L. Smith(4), M.K. Quinn(5)

1, 3, 4,
5: Dept. of Mechanical and Aerospace Engineering, The University of Manchester, UK
2: Dept. of Chemistry, The University of Manchester, UK