Andere Kunden interessierten sich auch für
![Spatially-Resolved Temperature Diagnostic for Supersonic Flow Using Cross-Beam Doppler-Limited Laser Saturation Spectroscopy]( "Spatially-Resolved Temperature Diagnostic for Supersonic Flow Using Cross-Beam Doppler-Limited Laser Saturation Spectroscopy")
Spatially-Resolved Temperature Diagnostic for Supersonic Flow Using Cross-Beam Doppler-Limited Laser Saturation Spectroscopy61,99 €![Remote Quantification of Smokestack Total Effluent Mass Flow Rates Using Imaging Fourier-Transfrom Spectroscopy]( "Remote Quantification of Smokestack Total Effluent Mass Flow Rates Using Imaging Fourier-Transfrom Spectroscopy")
Remote Quantification of Smokestack Total Effluent Mass Flow Rates Using Imaging Fourier-Transfrom Spectroscopy60,99 €![Efficient Low-Speed Flight in a Wind Field]( "Efficient Low-Speed Flight in a Wind Field")
Efficient Low-Speed Flight in a Wind Field61,99 €![Experimental Investigation of Oblique Wing Aerodynamics at Low Speed]( "Experimental Investigation of Oblique Wing Aerodynamics at Low Speed")
Experimental Investigation of Oblique Wing Aerodynamics at Low Speed63,99 €![Experimental and Theoretical Studies in Low Temperature Physics: Sublimation and Vapor Pressure of Ar 36 and the Combined Effects of Phonon Attenuatio]( "Experimental and Theoretical Studies in Low Temperature Physics: Sublimation and Vapor Pressure of Ar 36 and the Combined Effects of Phonon Attenuatio")
Experimental and Theoretical Studies in Low Temperature Physics: Sublimation and Vapor Pressure of Ar 36 and the Combined Effects of Phonon Attenuatio64,99 €![Collision Avoidance for UAVs Using Optic Flow Measurement with Line of Sight Rate Equalization and Looming]( "Collision Avoidance for UAVs Using Optic Flow Measurement with Line of Sight Rate Equalization and Looming")
Collision Avoidance for UAVs Using Optic Flow Measurement with Line of Sight Rate Equalization and Looming60,99 €![Flow Separation Prevention on a Turbine Blade in Cascade at Low Reynolds Number]( "Flow Separation Prevention on a Turbine Blade in Cascade at Low Reynolds Number")
Flow Separation Prevention on a Turbine Blade in Cascade at Low Reynolds Number63,99 €
This research advances a technique to simulate high temperature/high speed effects in a high speed/low temperature environment and to capture recession of the test article in three-dimensions. A method of fabricating dry ice test articles was developed, and the AFIT Mach 3 pressure-vacuum wind tunnel was used in combination with the dry ice test articles to collect three-dimensional ablation data for models of different shapes at stagnation pressures ranging from approximately 0.4 atm to 3 atm and stagnation temperatures equivalent to room temperature. High speed Schlieren photography was used for visualization, and the three dimensional shape change was quantified with sub-millimeter accuracy using laser dot photogrammetry. Experimental results for multiple shapes were compared to those computed using a computational model called ACFD. The ACFD model employed a finite-volume approach to solving the (3-D) Navier-Stokes equations with the gas assumed to be at equilibrium while employing an implicit solver accounting for the material response. By and large, the computational approach was validated for the conditions tested herein. Measurement of ablation rates at the stagnation point yielded approximate values of convective heat transfer rate when conduction through the solid is assumed negligible. The results of this analysis compared favorably to a variety of extensions of the Fay-Riddell correlation given in the literature. Paths for further research were selected and discussed.
Hinweis: Dieser Artikel kann nur an eine deutsche Lieferadresse ausgeliefert werden.
Hinweis: Dieser Artikel kann nur an eine deutsche Lieferadresse ausgeliefert werden.