About
I enjoy transforming theoretical concepts into practical tools. Currently maintaining…
Activity
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Is cutting and pasting from NASA's CEA code causing your pointing finger to become a workplace injury? Does having to repeat the same…
Is cutting and pasting from NASA's CEA code causing your pointing finger to become a workplace injury? Does having to repeat the same…
Shared by Jonathan French
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Forty years ago today, I walked into Chemical Systems Division as Research Propulsion Engineer, what I did not know at that time was this was not…
Forty years ago today, I walked into Chemical Systems Division as Research Propulsion Engineer, what I did not know at that time was this was not…
Liked by Jonathan French
Experience
Education
Publications
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Nozzle Acoustic Dynamics and Stability Modeling
Journal of Propulsion and Power
An eigensolver is used to calculate the acoustic modes of several rocket motors with steady flow effects. The nozzle damping is calculated by integrating the flux of unsteady energy through the nozzle's throat.
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UCDS Nozzle Acoustic Dynamics and Stability Modeling
American Institute of Aeronautics and Astronautics
Presents a new methodology for computing resonant acoustics in chambers with steady flow field effects, and for determining the overall impact on the combustion stability analysis.
Other authorsSee publication -
A Comparison of Nonlinear Combustion Stability Methods
American Institute of Aeronautics and Astronautics
A comparison of Culick's gas dynamics methodology with Flandro's energy balance approach for prediction of combustion stability limit cycle amplitudes.
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Linked Solid Rocket Motor Combustion Stability and Internal Ballistics Analysis
American Institute of Aeronautics and Astronautics
Comparison of nonlinear combustion stability analysis predictions with experiment.
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Solid Rocket Motor Grid Generation and CFD for Internal Ballistics Analysis
American Institute of Aeronautics and Astronautics
Presentation of automated 3D grid generation for solid rocket motor performance analysis, and accompanying CFD analysis.
Other authors -
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Improvements to the Linear Standard Stability Prediction Program (SSP)
American Institute of Aeronautics and Astronautics
Demonstrates how incorporating new linear stability theories into combustion stability analysis shifts solid rocket motor stability prediction toward motors being less stable. Also introduces automated 3D grid generation with accompanying acoustics analysis.
Other authorsSee publication -
Non-Linear Combustion Stability Prediction of SRMs using SPP / SSP
American Institute of Aeronautics and Astronautics
Details improvements to linear stability analysis, and demonstrates that Culick's gas dynamics methodology produces steep fronted waves, as found in Flandro's energy balance approach.
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Tangential Mode Instability of SRMs with Even and Odd Numbers of Slots
American Institute of Aeronautics and Astronautics
Using current linear combustion stability theory, demonstrated no distinction in combustion stability between solid rocket motors possessing even and odd numbers of slots.
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Analytic Evaluation of a Tangential Mode Instability in a Solid Rocket Motor
American Institute of Aeronautics and Astronautics
Investigation into a high frequency oscillation in an medium scale solid rocket motor.
Patents
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Scaleable acoustically-stable combustion chamber and design methods
Filed US US Patent App. 15/729,591
More activity by Jonathan
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Two years ago, amidst the throes of a mid-career crisis that had me debating whether I wanted to spend the rest of my working life doing only…
Two years ago, amidst the throes of a mid-career crisis that had me debating whether I wanted to spend the rest of my working life doing only…
Liked by Jonathan French
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I’m happy to share that I’m starting a new position as Technical Area Lead - Energetics at Raytheon!
I’m happy to share that I’m starting a new position as Technical Area Lead - Energetics at Raytheon!
Liked by Jonathan French
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Super excited about Hopper2! It's better than SN1 in so many ways, including dropping integration time from 3 months to 5 weeks. Huge shoutout to all…
Super excited about Hopper2! It's better than SN1 in so many ways, including dropping integration time from 3 months to 5 weeks. Huge shoutout to all…
Liked by Jonathan French
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AP-based composite propellants have been utilized for more than a half-century, but a modern fundamental dataset was lacking in the literature. To…
AP-based composite propellants have been utilized for more than a half-century, but a modern fundamental dataset was lacking in the literature. To…
Liked by Jonathan French
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https://lnkd.in/gyxnFTz
https://lnkd.in/gyxnFTz
Liked by Jonathan French
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And so begins our push to fully integrated first stage testing. Progressively we will test 1, 2, 3 then 4 engines simultaneously on TS-1 before the…
And so begins our push to fully integrated first stage testing. Progressively we will test 1, 2, 3 then 4 engines simultaneously on TS-1 before the…
Liked by Jonathan French
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