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Showing 1 to 20 of 36 for “"high-enthalpy"”.

  1. High-fidelity modeling of high-enthalpy plasma wind tunnels for hypersonic testing

    Submission published under a 24 month embargo labeled 'U of I Access', the embargo will last until 2027-08-01

    uiuc Repository record for High-fidelity modeling of high-enthalpy plasma wind tunnels for hypersonic testing (opens in a new tab)

  2. A Study of Direct Measuring Skin Friction Gages for High Enthalpy Flow Applications

    … gage for applications in three-dimensional, high-speed, high-enthalpy flows. Design conditions required favorable gage performance in the Arc-Heated Facilities at Arnold Engineering Development Center. Flow conditions are expected to be at Mach 3.4, with convective heat properties of h= 1,500 …

    vt Repository record for A Study of Direct Measuring Skin Friction Gages for High Enthalpy Flow Applications (opens in a new tab)

  3. Preliminary design of a high enthalpy plasma tunnel for atmospheric re-entry research

    … the response of the material as it is exposed to high reactive, high-temperature flow. The data collected from the experiments conducted at the facility will be used to verify computer models as well as material performance characteristics. This thesis describes the preliminary design process and …

    uiuc Repository record for Preliminary design of a high enthalpy plasma tunnel for atmospheric re-entry research (opens in a new tab)

  4. Skin Friction Sensor Design Methodology and Validation for High-Speed, High-Enthalpy Flow Applications

    … sensor capable of performing favorably in high-speed, high-enthalpy flow conditions, such as that found in atmospheric re-entry vehicles, scramjets, jet engines, material testing, and industrial processes. Fully understanding and optimizing these complex flows requires an understanding of …

    vt Repository record for Skin Friction Sensor Design Methodology and Validation for High-Speed, High-Enthalpy Flow Applications (opens in a new tab)

  5. Modeling of high enthalpy flows for hypersonic re-entry and ground-based arc-jet testing

    … presents a simulation framework for modeling high enthalpy ionized gas flows during planetary entry flights and ground-based arc-jet testing. The system of Favre-averaged Navier-Stokes equations in thermo-chemical non-equilibrium with Spalart-Allmaras turbulence closure is outlined, along with …

    uiuc Repository record for Modeling of high enthalpy flows for hypersonic re-entry and ground-based arc-jet testing (opens in a new tab)

  6. Prediction of flight measurements of high enthalpy nonequilibrium flow from a cubesat-class atmospheric probe

    Submission original under an indefinite embargo labeled 'Open Access'. The submission was exported from vireo on 2018-08-31 without embargo terms

    uiuc Repository record for Prediction of flight measurements of high enthalpy nonequilibrium flow from a cubesat-class atmospheric probe (opens in a new tab)

  7. Development and Ground Testing of Direct Measuring Skin Friction Gages for High Enthalpy Supersonic Flight Tests

    … skin friction gages were developed for a high-speed, high-temperature environment of the turbulent boundary layer in flows such as that in supersonic combustion ramjet (scramjet) engines, with a progression from free-jet ground tests to a design for an actual hypersonic scramjet-integrated …

    vt Repository record for Development and Ground Testing of Direct Measuring Skin Friction Gages for High Enthalpy Supersonic Flight Tests (opens in a new tab)

  8. An actively cooled floating element skin friction balance for direct measurement in high enthalpy supersonic flows

    … AMES Research Center. Flow conditions in the high enthalpy combustor models ranged from total pressures of 275-800 psia (1900-5550 kPa) and total temperatures from 5800-8400 R (3222-4667 K). This gives enthalpies in the range of 1700-3300 BTU/Ib<sub>m</sub> (3950-7660 KJ/kg) and simulated …

    vt Repository record for An actively cooled floating element skin friction balance for direct measurement in high enthalpy supersonic flows (opens in a new tab)

  9. Post-shock thermochemistry in hypervelocity CO2 and air flow

    This work represents ongoing efforts to study high-enthalpy carbon dioxide flows in anticipation of the upcoming Mars Science Laboratory (MSL) and future missions to the red planet. The work is motivated by observed anomalies between experimental and numerical studies in hypervelocity impulse …

    uiuc Repository record for Post-shock thermochemistry in hypervelocity CO2 and air flow (opens in a new tab)

  10. Retrograde melting in transition metal-silicon systems : thermodynamic modeling, experimental verification, and potential application

    … at temperatures above the binary eutectic. High enthalpy of formation of point defects in silicon leads to retrograde solubility for a number of solutes, including many 3d transition metals. The Ni-Si system is used to demonstrate that in silicon under supersaturated conditions, such solutes …

    mit Repository record for Retrograde melting in transition metal-silicon systems : thermodynamic modeling, experimental verification, and potential application (opens in a new tab)

  11. Experimental study of heat transfer to hypersonic nozzle walls

    The heat transfer rate from a high enthalpy gas to the walls of a diverging nozzle, through which the gas was flowing, has been experimentally determined. The experimental results are compared with the predictions of several theories for the heat transfer through a laminar boundary layer from a …

    rice Repository record for Experimental study of heat transfer to hypersonic nozzle walls (opens in a new tab)

  12. Design, construction and characterization of a wind tunnel

    … wind tunnels. The progress of the wind tunnel is highly related to the advancements in air crafts. Aircraft manufacturing has pushed the wind tunnel technology forward. Wind tunnels can be categorized by the wind speed limit differences, which are controlled by the mechanism of the driving …

    njit Repository record for Design, construction and characterization of a wind tunnel (opens in a new tab)

  13. Flameholding methods for compact hypersonic systems

    … hypersonic systems were characterized using high-speed pressure measurements and imaging in the high-enthalpy supersonic facility ACT-II. “Hypermixer” geometries consisting of tapered wedges with and without expansion-ramp vortex generators were tested in an axisymmetric Mach 2.6 flowpath to …

    uiuc Repository record for Flameholding methods for compact hypersonic systems (opens in a new tab)

  14. Validation of Conjugate Heat-Transfer Capability for Water- Cooled High-Speed Flows

    … are validated against existing data for three high speed water-cooled wind tunnel experiments: i) Air Force high-enthalpy nozzle test which recorded the increase in water coolant temperature, ii) Jet Propulsion Lab converging-diverging nozzle test for which nozzle and run-up were …

    embry-riddle Repository record for Validation of Conjugate Heat-Transfer Capability for Water- Cooled High-Speed Flows (opens in a new tab)

  15. Laser absorption spectroscopy for investigation of hypersonic propulsion

    … of the hypersonic flight environment. Generating high enthalpy conditions often produces a test gas with an altered chemical composition, which can influence combustion performance downstream. This dissertation first addresses this issue by characterizing the inflow gas in the ACT-II facility, …

    uiuc Repository record for Laser absorption spectroscopy for investigation of hypersonic propulsion (opens in a new tab)

  16. Optimization of enhancements to aluminum-based structural energetic materials

    … most often made of steel due to its low cost, high strength, good manufacturability, and ability to produce dense high-speed fragments. However, inert steel does not improve blast wave characteristics. In fact, it significantly reduces peak blast pressure and impulse as energy is expended in …

    uiuc Repository record for Optimization of enhancements to aluminum-based structural energetic materials (opens in a new tab)

  17. Conceptual design of nuclear systems for hydrogen production

    … reactor for providing heat and electricity for high temperature steam electrolysis and a hybrid electrolysis-chemical sulfur cycle. Also addressed is the sensitivity of production and efficiency of these cycles to process conditions. For a desired hydrogen distribution pressure of 3MPa, high

    mit Repository record for Conceptual design of nuclear systems for hydrogen production (opens in a new tab)

  18. Application of Ab-initio Quantum Chemistry Techniques to Hypersonic Flows for Plasma Blackout Alleviation

    … blocks communications with vehicles flying in a high-enthalpy flow environment. The ability to mitigate this issue can be useful from various re-entry vehicles to in-atmosphere hypersonic vehicles, especially with aerospace largely pushing into the hypersonic field across the industry. This …

    mit Repository record for Application of Ab-initio Quantum Chemistry Techniques to Hypersonic Flows for Plasma Blackout Alleviation (opens in a new tab)

  19. Design of Gages for Direct Skin Friction Measurements in Complex Turbulent Flows with Shock Impingement Compensation

    … disparate test conditions: 1) short-duration, high-enthalpy testing, 2) blow-down testing, and 3) flight testing. The resulting optimized gage designs were virtually tested against each set of nominal load conditions. The finalized designs each successfully met their respective test condition …

    vt Repository record for Design of Gages for Direct Skin Friction Measurements in Complex Turbulent Flows with Shock Impingement Compensation (opens in a new tab)

  20. Floating head skin friction gage measurements in supersonic flows

    … the skin friction coefficient in short duration, high enthalpy supersonic flows as well as long duration supersonic flows. The Macor model design yielded skin friction coefficient values near the expected value of 0.0014 when placed in a supersonic tunnel at both Mach 2.4 and Mach 3.0 and in a …

    vt Repository record for Floating head skin friction gage measurements in supersonic flows (opens in a new tab)

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