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1
Combustion-acoustic stability analysis for premixed gas turbine combustors
[Washington, D.C.] : [Springfield, Va.] : National Aeronautics and Space Administration ; [National Technical Information Service, distributor], 1995Format: Government Document Book
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2
Active combustion control for aircraft gas turbine engines
Cleveland, Ohio : Hanover, MD :; Cleveland, Ohio : Hanover, MD : National Aeronautics and Space Administration, Glenn Research Center ; Available from NASA Center for Aerospace Information, 2000Format: Government Document Book
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3
Combustion noise at elevated pressures in a liquid-fueled premixed combustor
[Washington, DC] : [Springfield, Va.] :; [Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration ; [National Technical Information Service, distributor], 1997Format: Government Document Book
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4
ASRM combustion instability studies
[Pasadena, Calif.?] : [Springfield, Va.] : Jet Propulsion Laboratory, California Institute of Technology ; [National Technical Information Service, distributor], 1992Format: Government Document Book
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5
A sectored-one-dimensional model for simulating combustion instabilities in premix combustors
Cleveland, Ohio : Hanover, MD : Springfield, VA :; Cleveland, Ohio : Hanover, MD : Springfield, VA : National Aeronautics and Space Administration, Glenn Research Center ; Available from NASA Center for Aerospace Information ; National Technical Information Service [distributor], 1999Format: Government Document Book
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6
Flow diagnostics, chemically reacting turbulent flow modeling and turbulent mixing : a summary of project studies in combustion
[Washington, DC] : [Springfield, Va.] : [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1995Format: Government Document Book
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7
Review of combustion-acoustic instabilities
[Washington, D.C.] : [Springfield, Va.] : National Aeronautics and Space Administration ; [National Technical Information Service, distributor], 1995Format: Government Document Book
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8
Advanced CFD methodology for fast transients encountered in nonlinear combustion instability problems : SBIR phase II final report (restricted circulation)
[Marshall Space Flight Center, Ala.] : [Springfield, Va.] : National Aeronautics and Space Administration, George C. Marshall Space Flight Center ; [National Technical Information Service, distributor], 1992Format: Government Document Book
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9
A fully implicit time accurate method for hypersonic combustion : application to shock-induced combustion instability
Cleveland, Ohio : [Springfield, Va.] : National Aeronautics and Space Administration, Lewis Research Center, Ohio Aerospace Institute, Institute for Computational Mechanics in Propulsion ; [National Technical Information Service, distributor], 1994Format: Government Document Book
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10
Hybrid propulsion for launch vehicle boosters : a program status update
Washington, D.C. : [Springfield, Va.] : [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1995Format: Government Document Book
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11
Solid-propellant rocket motor internal ballistics performance variatio analysis (phase five) : final report
Auburn, Ala. : [Washington, DC] : [Springfield, Va.] : Engineering Experiment Station, Auburn University ; [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1980Format: Government Document Book
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12
Sensitivity of combustion-acoustic instabilities to boundary conditions for premixed gas turbinecombustors
[Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration ; [National Technical Information Service, distributor], 1995Format: Government Document Book
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