1–20 of 39 hits
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    Quantification of Infinite Line Pressure Probe Response to Shocks and Detonation Waves

    Naples, Andrew / Hoke, John L. / Schauer, Frederick R. | AIAA | 2018

    Quantification of Infinite Line Pressure Probe Response to Shocks and Detonation Waves (AIAA 2018-1886)

    Naples, Andrew / Hoke, John L. / Schauer, Frederick R. | British Library Conference Proceedings | 2018

    Quasi-2D Simulations of Nozzled Rotating Detonation Engines with the Method of Characteristics

    Fievisohn, Robert / Hoke, John L. / Schauer, Frederick R. | AIAA | 2018

    Quasi-2D Simulations of Nozzled Rotating Detonation Engines with the Method of Characteristics (AIAA 2018-0881)

    Fievisohn, Robert / Hoke, John L. / Schauer, Frederick R. | British Library Conference Proceedings | 2018

    Velocimetry Measurements using Structured Light-Field Focusing in a Rotating Detonation Engine

    Sosa, Jonathan / Ahmed, Kareem / Hoke, John L. et al. | AIAA | 2018

    Parameter Impact on Heat Flux in a Rotating Detonation Engine

    Meyer, Samuel J. / Polanka, Marc D. / Schauer, Frederick R. et al. | AIAA | 2018

    Hydrocarbon Fuel Absorption Measurement in Rotating Detonation Engine

    Cho, Kevin Y. / Sell, Brian / Hoke, John L. et al. | AIAA | 2018

    Design of a Premixed Fuel-Oxidizer System to Prevent Flashback in a Rotating Detonation Engine

    Andrus, Ionio Q. / King, Paul / Polanka, Marc D. et al. | AIAA | 2016

    Mach Disk Pressure Measurement Technique within Rotating Detonation Engine

    Codoni, Joshua R. / Cho, Kevin Y. / Hoke, John L. et al. | AIAA | 2016

    Parameter Impact on Heat Flux in a Rotating Detonation Engine (AIAA 2018-0400)

    Meyer, Samuel J. / Polanka, Marc D. / Schauer, Frederick R. et al. | British Library Conference Proceedings | 2018

    Characterization of a Premixed Laboratory Scale Pulsed Detonation Burner

    Fernelius, Mark / Sell, Brian / Moosmann, Kaitlin J. et al. | AIAA | 2018

    Temperature Estimates of Exhaust Plumes from a Turbine Driven by Pulsed Detonations

    Rankin, Brent A. / Gore, Jay P. / Hoke, John L. et al. | AIAA | 2014

    Increasing Reliability of a Two-Stroke Internal Combustion Engine for Dynamically Changing Altitudes

    Crosbie, Steven C. / Polanka, Marc D. / Litke, Paul J. et al. | AIAA | 2013

    Design and Testing of a Micro-Scale Wave Rotor System

    Lapp, Kevin P. / Polanka, Marc D. / McClearn, Michael J. et al. | AIAA | 2017

    Small Turbojet Altitude Test Facility with Two Stage Turbocharger Inlet Air Cooling

    Grannan, Nicholas D. / Moosmann, Kaitlin J. / Hoke, John L. et al. | AIAA | 2018

    A Disk Rotating Detonation Engine Part 2: Operation

    McClearn, Michael J. / Schauer, Frederick R. / Huff, Riley et al. | AIAA | 2018

    A Disk Rotating Detonation Engine Part 1:Design and Buildup

    Huff, Riley / Polanka, Marc D. / McClearn, Michael J. et al. | AIAA | 2018

    Small Turbojet Altitude Test Facility with Two Stage Turbocharger Inlet Air Cooling (AIAA 2018-2119)

    Grannan, Nicholas D. / Moosmann, Kaitlin J. / Hoke, John L. et al. | British Library Conference Proceedings | 2018