Results 51 to 60 of about 101,352 (285)

Historical review and future perspectives for Pilot Transonic Wind Tunnel of IAE [PDF]

open access: yesJournal of Aerospace Technology and Management, 2009
The Pilot Transonic Wind Tunnel of Institute of Aeronautics and Space (PTT Pilot Transonic Wind Tunnel) is an important result of a tremendous effort to install a high speed wind tunnel complex (TTS acronyms for Transonic and Supersonic Tunnels, in ...
João Batista P. Falcão Filho   +2 more
doaj  

Electric arc device for heating gases Patent [PDF]

open access: yes, 1966
Electric arc device for minimizing electrode ablation and heating gases to supersonic or hypersonic wind tunnel ...
Carlson, W. C. A., Sorensen, C. E.
core   +1 more source

Evaluation of discontinuity treatment in intrusive polynomial chaos for uncertainty quantification of a nozzle flow in CFD

open access: yesJournal of Fluid Science and Technology, 2020
Stochastic flow simulation methods based on the polynomial chaos expansion (PCE) are developed and verified to quantify the propagation of a geometric uncertainty of a quasi-one dimensional flow in a supersonic wind tunnel.
Koji MIYAJI, Takumi INOUE
doaj   +1 more source

The Influence of Nozzle Geometry on Corner Flows in Supersonic Wind Tunnels [PDF]

open access: yesAIAA Scitech 2019 Forum, 2019
In supersonic flows, the separation in streamwise corners is a significant and widely encountered problem which can not be reliably predicted with the numerical methods commonly used in industry. The few previous studies on this topic have suggested conflicting corner flow topologies.
Sabnis, K   +3 more
openaire   +2 more sources

Experimental and numerical investigation of an air to air supersonic ejector for propulsion of a small supersonic wind tunnel

open access: yes, 2015
The article deals with experimental and numerical investigation of an air to air supersonic ejector with twelve primary nozzles. The ejector is supposed to be used for propulsion of a small experimental supersonic wind tunnel which is situated in ...
J. Kracík, V. Dvorák
semanticscholar   +1 more source

Numerical and Experimental Validation of a Supersonic Mixing Layer Facility

open access: yesApplied Sciences, 2022
The design of a supersonic-supersonic mixing layer facility was motivated by the need for a benchmark experimental platform to study the physical phenomena underlying supersonic mixing layers.
Yudong Li   +4 more
doaj   +1 more source

Deduction of temperature fluctuations in transient compression wind tunnels using incompressible turbulent flow data [PDF]

open access: yes, 2009
Wind tunnels and other aero-thermal experimental facilities are likely to make a contribution to the optimisation of energy and propulsion systems for the foreseeable future.
Buttsworth, D. R., Widodo, A.
core   +2 more sources

FPGA-based embedded system for wind tunnel variable-geometry nozzle positioning [PDF]

open access: yesScientific Technical Review, 2019
Over the last few decades, the accuracy requirements for wind tunnel testing have become much more stringent as aircraft industry strives to achieve the best performance of their products. Investments in advanced capabilities are necessary to obtain more
Ilić Biljana, Milosavljević Mirko
doaj  

Short-duration, transonic flow, variable-porosity test section [PDF]

open access: yes, 1970
Short-duration test facility obtains extremely high Reynolds number flows in subsonic, transonic, and supersonic speed ranges, and aids in solving Reynolds number-dependent aerodynamic and thermodynamic problems in design and testing of large, high speed
Davis, J. W., Hill, O. E.
core   +1 more source

Flow visualization techniques, new developments and modernization of the existing Schlieren system in the Trisonic Wind Tunnel [PDF]

open access: yesINCAS Bulletin, 2011
Schlieren flow visualization methods are an important part of high speed wind tunnel testing, being a fast and reliable method of graphically presenting complex dynamic phenomena that occur in high subsonic, transonic and supersonic regimes.
Marius PANAIT
doaj   +1 more source

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