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Dive into the research topics where Jesse R. Maxwell is active.

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Featured researches published by Jesse R. Maxwell.


55th AIAA Aerospace Sciences Meeting | 2017

Shapeable Inlet Manifold for Hypersonic Scramjet

Jesse R. Maxwell; Gabriel B. Goodwin

A shapeable inlet manifold for a hypersonic scramjet includes an inlet lower cowling; a mount surface; and an inlet stream surface movably coupled to the mount surface, wherein the inlet lower cowling and the inlet stream surface define an opening of the shapeable inlet manifold allowing fluid flow therethrough. The inlet stream surface has first and second dispositions relative to the lower cowling defining first and second shapes of the opening, thereby providing respective first and second flow characteristics through the inlet manifold during flight.


AIAA SPACE and Astronautics Forum and Exposition | 2017

Morphable Hypersonic Waverider and Trajectory Optimized for Atmospheric Entry

Jesse R. Maxwell; Austin A. Phoenix


53rd AIAA/SAE/ASEE Joint Propulsion Conference | 2017

Performance analysis of a hypersonic scramjet engine with a morphable waverider inlet

Gabriel B. Goodwin; Jesse R. Maxwell


2018 AIAA Aerospace Sciences Meeting | 2018

Dynamic Depletion and Test Section Conditions Model for Blow-Down Supersonic Wind Tunnel

Jesse R. Maxwell


Volume 2: Modeling, Simulation and Control of Adaptive Systems; Integrated System Design and Implementation; Structural Health Monitoring | 2017

Morphing High-Temperature Surfaces for Shapeable Hypersonic Waverider Vehicles

Austin A. Phoenix; Jesse R. Maxwell; Gabriel B. Goodwin


33rd AIAA Aerodynamic Measurement Technology and Ground Testing Conference | 2017

Flow Quality Numerical Characterization for Cold Adjustable Supersonic Wind Tunnel

Jesse R. Maxwell; Gabriel B. Goodwin


46th AIAA Thermophysics Conference | 2016

Two Phase Thermal Protection of the Hypersonic Leading Edge

Jesse R. Maxwell; Triem T. Hoang


2018 Fluid Dynamics Conference | 2018

Large Eddy Simulation of Continuously Adjustable Hypersonic Wind Tunnel

Jesse R. Maxwell; Gabriel B. Goodwin


2018 Aerodynamic Measurement Technology and Ground Testing Conference | 2018

Correction: Extended Model for Dynamic Depletion and Test Section Conditions for a Blow-Down Hypersonic Wind Tunnel

Jesse R. Maxwell; Gabriel B. Goodwin


2018 AIAA/AHS Adaptive Structures Conference | 2018

The Mach 5 to 3.5 Morphing Waverider Optimal Actuation Location Selection

Austin A. Phoenix; Jesse R. Maxwell

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Gabriel B. Goodwin

United States Naval Research Laboratory

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Austin A. Phoenix

United States Naval Research Laboratory

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Triem T. Hoang

United States Naval Research Laboratory

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Deborah Zakar

United States Naval Research Laboratory

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Robert W. Baldauff

United States Naval Research Laboratory

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Timothy D. Holman

United States Naval Research Laboratory

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