In recent years. measurement techniques at real-flight Reynolds numbers using real airplanes and high Reynolds number cryogenic wind tunnels like European Transonic Windtunnel (ETW) has been actively developed also in European countries. In this paper, the overview of the Advanced ln-Flight Measurement Techniques (AIM) as European projects and the obtained knowledge through at the in-flight PSP measurement are reported. In addition, the high Reynolds number testing including TSP performed in cryogenic wind tunnels such as ETW are presented
The identification of laminar-turbulent boundary layer transition on models in cryogenic wind tunnel...
The pressure sensitive paint (PSP system is an optical measurement technique to investigate absolute...
The pressure sensitive paint intensity and lifetime system (PSP) is an optical measurement technique...
Future generations of aircraft will be developed applying “High Reynolds Number Design”, using advan...
The present paper addresses the development, qualification trials and application of some non-intrus...
Nowadays, advanced optical measurement methods for wind tunnel or laboratory applications become mor...
Advanced optical measurement techniques are beneficial compared to classical sensor measurements in ...
I will present the microphone array measurement technique which was advanced at the DLR Göttingen fo...
In-flight testing of aircraft requires the measurement of many different parameters to ensure the ai...
With the goal of studying Natural Laminar Flow (NLF) wings for future ‘green’ transport aircraft, th...
Making new advanced optical measurement techniques that have their roots in wind tunnel or laborator...
The present paper addresses the development,qualification trials and application of somemodern measu...
The presentation will briefly present the state-of-the-art of image based measurement techniques for...
Cryogenic, high-Reynolds number testing has been in use for approximately 40 years. This testing cap...
In 2020, the first Pressure Sensitive Paint (PSP) test campaign within the research initiative “Uns...
The identification of laminar-turbulent boundary layer transition on models in cryogenic wind tunnel...
The pressure sensitive paint (PSP system is an optical measurement technique to investigate absolute...
The pressure sensitive paint intensity and lifetime system (PSP) is an optical measurement technique...
Future generations of aircraft will be developed applying “High Reynolds Number Design”, using advan...
The present paper addresses the development, qualification trials and application of some non-intrus...
Nowadays, advanced optical measurement methods for wind tunnel or laboratory applications become mor...
Advanced optical measurement techniques are beneficial compared to classical sensor measurements in ...
I will present the microphone array measurement technique which was advanced at the DLR Göttingen fo...
In-flight testing of aircraft requires the measurement of many different parameters to ensure the ai...
With the goal of studying Natural Laminar Flow (NLF) wings for future ‘green’ transport aircraft, th...
Making new advanced optical measurement techniques that have their roots in wind tunnel or laborator...
The present paper addresses the development,qualification trials and application of somemodern measu...
The presentation will briefly present the state-of-the-art of image based measurement techniques for...
Cryogenic, high-Reynolds number testing has been in use for approximately 40 years. This testing cap...
In 2020, the first Pressure Sensitive Paint (PSP) test campaign within the research initiative “Uns...
The identification of laminar-turbulent boundary layer transition on models in cryogenic wind tunnel...
The pressure sensitive paint (PSP system is an optical measurement technique to investigate absolute...
The pressure sensitive paint intensity and lifetime system (PSP) is an optical measurement technique...