We demonstrate a new variation of molecular-tagging velocimetry for hypersonic ows based
on laser-induced uorescence. A thin line of nitric-oxide molecules is excited with a laser …

IN HYPERSONIC flow computations, it is a key issue to predict surface heating accurately.
However, it is still challenging to compute hypersonic flows, because there are always …

Hydroxyl tagging velocimetry (HTV) measurements of velocity were made in a Mach 2 (M 2)
flow with a wall cavity. In the HTV method, ArF excimer laser (193 nm) beams pass through a …

Interference heating effects generated by a blunt fin-type protuberance on a flat plate
exposed to a hypersonic flow have been investigated experimentally and numerically …

In order to apply the air fin successfully and ensure the maneuverability of hypersonic
vehicle, a key problem to be studied urgently is the heat flux brought by the fin mounting …

Shock-wave–boundary-layer interaction is one of the most important phenomena in
hypersonic flights due to its ubiquitous presence and its extreme effects on the …

A detailed comparison between computations and experiments is given for Mach 6 flow over
a straight cone with a highly swept fin. Five cases are simulated that vary the cone nose …

Hydroxyl-tagging-velocimetry measurements were made throughout the compressible
flowfield of a Mach 2 air flow over a cavity. The supersonic flowfield simulates the pilot …

Results of refined RANS-based numerical simulation of shock wave/turbulent boundary
layer interaction induced by a blunted fin mounted on a flat plate are presented. The RANS …

In this paper, a new type of molecular tagging velocimetry based on NH fluorescence was
developed and validated for the velocity measurements of a high-enthalpy rarefied gas wind …