[書籍][B] Pressure and temperature sensitive paints
The first edition of the book “Pressure and Temperature Sensitive Paints” published by
Springer in 2005 summarizes the early development of pressure-and temperature-sensitive …
Springer in 2005 summarizes the early development of pressure-and temperature-sensitive …
Characterization of an ultrathin polymer optode and its application to temperature sensors based on luminescent europium complexes
M Mitsuishi, S Kikuchi, T Miyashita… - Journal of Materials …, 2003 - pubs.rsc.org
This paper focuses on an ultrathin polymer optode containing europium complexes (p (DDA-
Eu (TTA) 3Phen)). Ultrathin films were prepared by the Langmuir–Blodgett (LB) technique; a …
Eu (TTA) 3Phen)). Ultrathin films were prepared by the Langmuir–Blodgett (LB) technique; a …
Infrared thermography for boundary layer transition measurements
Infrared thermography has been successfully adopted in the field of flow diagnostics over
the last decades. Detecting the laminar–turbulent boundary layer transition through …
the last decades. Detecting the laminar–turbulent boundary layer transition through …
Transition detection by temperature sensitive paint at cryogenic temperatures in the European Transonic Wind tunnel (ETW)
U Fey, RH Engler, Y Egami, Y Iijima… - … on Instrumentation in …, 2003 - ieeexplore.ieee.org
The identification of laminar-turbulent boundary layer transition on wind tunnel models
provides essential data for modern wing design. However, simulating true flight Reynolds …
provides essential data for modern wing design. However, simulating true flight Reynolds …
A robust method for reliable transition detection in temperature-sensitive paint data
M Costantini, U Henne, S Risius, C Klein - Aerospace Science and …, 2021 - Elsevier
This work presents a method to automatically detect boundary-layer transition on
thermographic images of aerodynamic surfaces, acquired using the temperature-sensitive …
thermographic images of aerodynamic surfaces, acquired using the temperature-sensitive …
Extraction of skin friction topology of turbulent wedges on a swept wing in transonic flow from surface temperature images
T Liu, DM Salazar, J Crafton, AN Watkins - Experiments in Fluids, 2021 - Springer
This paper describes a first-order approximate method of extracting the skin friction topology
of turbulent wedges from temperature sensitive paint (TSP) images on a NASA Common …
of turbulent wedges from temperature sensitive paint (TSP) images on a NASA Common …
Surface pressure measurement in a cryogenic wind tunnel by using luminescent coating
K Asai, H Kanda, CT Cunningham… - ICIASF'97 Record …, 1997 - ieeexplore.ieee.org
In recent experiments, we demonstrated the feasibility of using luminescent coatings for
surface pressure measurement in a cryogenic wind tunnel. This technique is based on a …
surface pressure measurement in a cryogenic wind tunnel. This technique is based on a …
Nonadiabatic surface effects on transition measurements using temperature-sensitive paints
M Costantini, U Fey, U Henne, C Klein - AIAA Journal, 2015 - arc.aiaa.org
Tests were conducted at the Cryogenic Ludwieg-Tube Göttingen to investigate the influence
on onset of boundary-layer transition of thermal gradients on the model surface, whereby the …
on onset of boundary-layer transition of thermal gradients on the model surface, whereby the …
Platinum octaetylporphyrin based planar optodes combined with an UV-LED excitation light source: An ideal tool for high-resolution O2 imaging in O2 depleted …
K Oguri, H Kitazato, RN Glud - Marine Chemistry, 2006 - Elsevier
A planar optode system based on an O2 quenchable luminophore platinum (II) 2, 3, 7, 8, 12,
13, 17, 18-octaethyl-21H, 23H-porphyrin (PtOEP) and UV-light emitting diodes (LEDs) was …
13, 17, 18-octaethyl-21H, 23H-porphyrin (PtOEP) and UV-light emitting diodes (LEDs) was …
Boundary-layer transition on cones at angle of attack in a Mach-6 quiet tunnel
E Swanson, S Schneider - … Meeting Including the New Horizons Forum …, 2010 - arc.aiaa.org
A series of experiments have been conducted to study hypersonic boundary-layer transition
over 7 cones at angle of attack in the Purdue Boeing/AFOSR Mach-6 Quiet Tunnel. The …
over 7 cones at angle of attack in the Purdue Boeing/AFOSR Mach-6 Quiet Tunnel. The …