Results 81 to 90 of about 15,113 (249)
This article explores how the integration of a thin shell, combined with optimized surface chemistry, enables the design of photodiodes based on short‐wave infrared HgTe nanocrystals. These photodiodes achieve an open‐circuit voltage greater than half the optical bandgap, which drastically reduces dark current. The article also explores the integration
Albin Colle +17 more
wiley +1 more source
Additional correction of 4 percent Saturn 5 protuberance test data [PDF]
Transonic wind tunnel background noise measurement for analysis of Saturn 5 model protuberance test ...
Mc Canless, G. F., Jr.
core +1 more source
Experimental program to investigate transonic flow around protuberances [PDF]
Transient and steady state aerodynamic flow of turbulent boundary layers are investigated for generalized cylindrical projections and several specific configurations used on the Saturn 5 launch vehicle.
Robertson, J. E.
core +1 more source
A Comparative Study on Early‐Stage Icing Evaluation Techniques for Passive Ice Protection Systems
This study addresses the lack of standardized methodologies for evaluating the early‐stage icing performance of passive ice protection systems. A unified experimental protocol is proposed and applied to representative hydrophilic and hydrophobic surfaces under controlled conditions.
Lorenzo Facco +4 more
wiley +1 more source
Remote detection of boundary-layer transition by an optical system [PDF]
This instrument development program was funded because of the urgent need to measure boundary-layer transition in wind tunnels. In the course of this development program, a prototype was designed, built, and tested.
Azzazy, Medhat +2 more
core +1 more source
Measured unsteady transonic aerodynamic characteristics of an elastic supercritical wing with an oscillating control surface [PDF]
Transonic steady and unsteady aerodynamic data were measured on a large elastic wing in the NASA Langley Transonic Dynamics Tunnel. The wing had a supercritical airfoil shape and a leading-edge sweepback of 28.8 deg.
Brooks J. D. +7 more
core +2 more sources
In this study, we report a resistive‐type strain sensor fabricated using single‐walled CNTs, are used layer using the pray technique to deposit as conductive, and UV‐resin was spin‐coated as a protection layer. The sensor functioned in harsh temperature variation conditions from −50°C to 125°C without deterioration.
Jagan Singh Meena +4 more
wiley +1 more source
The shock wave boundary layer interaction on the suction side of a transonic compressor blade is one of the main objectives of the TFAST project (Transition Location Effect on Shock Wave Boundary Layer Interaction).
MICHAŁ PIOTROWICZ +2 more
doaj +1 more source
Experimental program for the investigation of transonic flow around protuberances in the AEDC-16T wind tunnel facility [PDF]
Steady and fluctuating airloads on protuberance and surrounding structure of transonic propulsion wind tunnel ...
Robertson, J. E.
core +1 more source
Transonic Wind Tunnel Testing [PDF]
Bernhard H. Goethert, J. Lukasiewicz
openaire +1 more source

