High-speed PLIF imaging of hypersonic transition over discrete cylindrical roughness
Transitional flow over cylindrical protuberances attached to a flat plate has been studied in a
hypersonic wind tunnel. The tests were performed in the 31-Inch Mach 10 Air Tunnel at …
hypersonic wind tunnel. The tests were performed in the 31-Inch Mach 10 Air Tunnel at …
Fluorescence visualization of hypersonic flow past triangular and rectangular boundary-layer trips
Planar laser-induced fluorescence (PLIF) flow visualization has been used to investigate the
hypersonic flow of air over surface protrusions that are sized to force laminar-to-turbulent …
hypersonic flow of air over surface protrusions that are sized to force laminar-to-turbulent …
NO PLIF study of hypersonic transition over a discrete hemispherical roughness element
Nitric oxide (NO) planar laser-induced fluorescence (PLIF) has been use to investigate the
hypersonic flow over a flat plate with and without a 2-mm (0.08-in) radius hemispherical trip …
hypersonic flow over a flat plate with and without a 2-mm (0.08-in) radius hemispherical trip …
PLIF visualization of active control of hypersonic boundary layers using blowing
Planar laser-induced fluorescence (PLIF) imaging was used to visualize the boundary layer
flow on a 1/3-scale Hyper-X forebody model. The boundary layer was perturbed by blowing …
flow on a 1/3-scale Hyper-X forebody model. The boundary layer was perturbed by blowing …
Planar laser-induced fluorescence (PLIF) investigation of hypersonic flowfields in a Mach 10 wind tunnel
P Danehy, JA Wilkes, DW Alderfer, SB Jones… - 25th AIAA Aerodynamic …, 2006 - arc.aiaa.org
Planar laser-induced fluorescence (PLIF) of nitric oxide (NO) was used to visualize four
different hypersonic flowfields in the NASA Langley Research Center 31-Inch Mach 10 Air …
different hypersonic flowfields in the NASA Langley Research Center 31-Inch Mach 10 Air …
Hypersonic laminar boundary layer velocimetry with discrete roughness on a flat plate
This material is declared a work of the US Government and is not subject to copyright
protection in the United States. spatial depth of 0.5-mm. Temperature sensitive paint (TSP) …
protection in the United States. spatial depth of 0.5-mm. Temperature sensitive paint (TSP) …
MHz-rate nitric oxide planar laser-induced fluorescence imaging in a Mach 10 hypersonic wind tunnel
Nitric oxide planar laser-induced fluorescence (NO PLIF) imaging at repetition rates as high
as 1MHz is demonstrated in the NASA Langley 31 in. Mach 10 hypersonic wind tunnel …
as 1MHz is demonstrated in the NASA Langley 31 in. Mach 10 hypersonic wind tunnel …
Fluorescence imaging and streakline visualization of hypersonic flow over rapid prototype wind-tunnel models
The use of planar laser-induced fluorescence (PLIF) of nitric oxide (NO) was inves-tigated
for use in visualizing wake flowfields downstream of rapid prototyping models in a …
for use in visualizing wake flowfields downstream of rapid prototyping models in a …
PLIF imaging of mean temperature and pressure in a supersonic bluff wake
ER Lachney, NT Clemens - Experiments in Fluids, 1998 - Springer
Planar laser-induced fluorescence (PLIF) of seeded nitric oxide was used to obtain mean 2-
D temperature and pressure fields in the near-wake region of a thick flat plate in a Mach 3 …
D temperature and pressure fields in the near-wake region of a thick flat plate in a Mach 3 …
Nitric-Oxide Ionization Induced Flow Tagging and Imaging for Near-Surface Velocimetry in Hypersonic Boundary Layers
In this paper, the authors describe an experimental demonstration of Nitric-oxide ionization
induced Flow Tagging and Imaging (NiiFTI) in near-surface velocimetry applications. The …
induced Flow Tagging and Imaging (NiiFTI) in near-surface velocimetry applications. The …