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Andrew D. Cutler
Researcher at George Washington University
Publications - 163
Citations - 2589
Andrew D. Cutler is an academic researcher from George Washington University. The author has contributed to research in topics: Supersonic speed & Combustor. The author has an hindex of 27, co-authored 158 publications receiving 2353 citations. Previous affiliations of Andrew D. Cutler include Langley Research Center & Joint Institute for Nuclear Research.
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Journal ArticleDOI
Coherent Anti-Stokes Raman Spectroscopic Thermometry in a Supersonic Combustor
Andrew D. Cutler,Paul M. Danehy,R. R. Springer,Sean O'Byrne,Diego P. Capriotti,Richard DeLoach +5 more
TL;DR: In this paper, the authors used coherent anti-Stokes Raman spectroscopy to acquire data for the validation of computational fluid dynamics codes used in the design of supersonic combustors.
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Dual-Pump Coherent Anti-Stokes Raman Scattering Measurements in a Supersonic Combustor
TL;DR: The dual-pump coherent anti-Stokes Raman scattering (CARS) method was used to measure temperature and the mole fractions of N 2 and O 2 in a supersonic combustor.
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Large-Eddy/Reynolds-Averaged Navier–Stokes Simulations of Reactive Flow in Dual-Mode Scramjet Combustor
Jesse A. Fulton,Jack R. Edwards,Hassan Hassan,James C. McDaniel,Christopher P. Goyne,Robert D. Rockwell,Andrew D. Cutler,Craig T. Johansen,Paul M. Danehy +8 more
TL;DR: In this paper, a hybrid large-eddy simulation/Reynolds-averaged Navier-Stokes method is used, with special attention focused on capturing facility-specific effects, such as asymmetric inflow temperature distributions, on flow development within the combustor.
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Mixing of swirling jets in a supersonic duct flow
Donna K. Kraus,Andrew D. Cutler +1 more
TL;DR: In this article, an experiment was conducted to determine whether the addition of swirl will improve the mixing of a supersonic jet of fuel simulant (helium or air) injected at 30 deg to the wall into a confined Mach 2 airflow.
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The relaxation of a turbulent boundary layer in an adverse pressure gradient
TL;DR: In this paper, an adverse pressure gradient is imposed upon the boundary layer to bring it into equilibrium, and the pressure gradient was adjusted so as to bring the Clauser parameter G down to a value of about 11.4.