3D rocket combustor acoustics model /
| Main Authors: | Priem, Richard J. (Author), Breisacher, Kevin J. (Author) |
|---|---|
| Format: | Government Document eBook |
| Language: | English |
| Published: |
[Washington, D.C.] :
NASA,
[July 1992]
|
| Series: | NASA technical memorandum ;
105734. |
| Subjects: | |
| Online Access: | https://purl.fdlp.gov/GPO/gpo195838 |
Similar Items
Low-power ion propulsion for small spacecraft /
by: Patterson, Michael J., 1959-, et al.
Published: (1997)
by: Patterson, Michael J., 1959-, et al.
Published: (1997)
An incidence loss model for wave rotors with axially aligned passages /
by: Paxson, Daniel E.
Published: (1998)
by: Paxson, Daniel E.
Published: (1998)
Computational ion optics design evaluations /
by: Malone, Shane P., et al.
Published: (2004)
by: Malone, Shane P., et al.
Published: (2004)
Full-scale turbofan engine noise-source separation using a four-signal method /
by: Hultgren, Lennart S. (Lennart Sven), et al.
Published: (2016)
by: Hultgren, Lennart S. (Lennart Sven), et al.
Published: (2016)
Bleed cycle propellant pumping in a gas-core nuclear rocket engine system /
by: Kascak, Albert F., et al.
Published: (1972)
by: Kascak, Albert F., et al.
Published: (1972)
Revolutionary vertical lift technology (RVLT) side-by-side hybrid concept vehicle powertrain dynamic model /
by: Bianco, Santino J.
Published: (2021)
by: Bianco, Santino J.
Published: (2021)
Ejector enhanced pulsejet based pressure gain combustors : an old idea with a new twist /
by: Paxson, Daniel E.
Published: (2005)
by: Paxson, Daniel E.
Published: (2005)
A control strategy for turbine electrified energy management /
by: Kratz, Jonathan L., et al.
Published: (2019)
by: Kratz, Jonathan L., et al.
Published: (2019)
Introducing the VRT gas turbine combustor /
by: Melconian, Jerry O.
Published: (1990)
by: Melconian, Jerry O.
Published: (1990)
A comparison of combustor-noise models /
by: Hultgren, Lennart S. (Lennart Sven)
Published: (2012)
by: Hultgren, Lennart S. (Lennart Sven)
Published: (2012)
Separating direct and indirect turbofan engine combustion noise while estimating post-combustion (post-flame) residence time using the correlation function /
by: Miles, Jeffrey H. (Jeffrey Hilton)
Published: (2011)
by: Miles, Jeffrey H. (Jeffrey Hilton)
Published: (2011)
Acoustical and flowfield characterization of a scaled tabletop rocket /
Published: (2001)
Published: (2001)
Acoustical and flowfield characterization of a scaled tabletop rocket /
by: Kandula, Max
Published: (2001)
by: Kandula, Max
Published: (2001)
Comparison of high aspect ratio cooling channel designs for a rocket combustion chamber with development of an optimized design /
by: Wadel, Mary F.
Published: (1998)
by: Wadel, Mary F.
Published: (1998)
6670-newton attitude-control thruster using hydrogen-oxygen propellant /
by: Gordon, Larry H.
Published: (1977)
by: Gordon, Larry H.
Published: (1977)
A simplified model for detonation based pressure-gain combustors /
by: Paxson, Daniel E.
Published: (2010)
by: Paxson, Daniel E.
Published: (2010)
Examination of the structural response of the Orion European service module to reverberant and direct field acoustic testing /
by: McNelis, Mark E.
Published: (2017)
by: McNelis, Mark E.
Published: (2017)
Electric propulsion options for 10 kW class earth space missions /
by: Patterson, Michael J., 1959-
Published: (1989)
by: Patterson, Michael J., 1959-
Published: (1989)
Electric propulsion options for 10 kW class earth space missions /
by: Patterson, Michael J., 1959-
Published: (1989)
by: Patterson, Michael J., 1959-
Published: (1989)
Flame tube NOx emissions using a lean-direct-wall-injection combustor concept /
by: Tacina, Robert R.
Published: (2001)
by: Tacina, Robert R.
Published: (2001)
Transfer-function determination for infinite-tube-probe pressure transducers with application to turbofan core/combustor noise /
by: Boyle, Devin K., et al.
Published: (2019)
by: Boyle, Devin K., et al.
Published: (2019)
Acoustic database for turbofan engine core-noise sources, volume I, final report /
by: Gordon, Grant
Published: (2015)
by: Gordon, Grant
Published: (2015)
Current status of post-combustor trace chemistry modeling and simulation at NASA Glenn Research Center /
by: Wey, Thomas
Published: (2003)
by: Wey, Thomas
Published: (2003)
Advanced liquid rockets /
by: Schneider, Stephen J.
Published: (1992)
by: Schneider, Stephen J.
Published: (1992)
The NASA low thrust propulsion program /
by: Stone, James R.
Published: (1989)
by: Stone, James R.
Published: (1989)
The NASA low thrust propulsion program /
by: Stone, James R.
Published: (1989)
by: Stone, James R.
Published: (1989)
Development of a gas-fed pulse detonation research engine /
by: Litchford, R. J.
Published: (2001)
by: Litchford, R. J.
Published: (2001)
One-third-octave analysis of core/combuster-noise measurements for the DGEN aeropropulsion research turbofan with application to noise prediction /
by: Hultgren, Lennart S. (Lennart Sven), et al.
Published: (2019)
by: Hultgren, Lennart S. (Lennart Sven), et al.
Published: (2019)
Flame radiation and liner heat transfer in a tubular-can combustor /
by: Claus, Russell W.
Published: (1984)
by: Claus, Russell W.
Published: (1984)
Flow processes in overexpanded chemical rocket nozzles.
by: Schmucker, Robert H.
Published: (1984)
by: Schmucker, Robert H.
Published: (1984)
NASA one-dimensional combustor simulation : user manual for S1D_ML /
by: Stueber, Thomas J., et al.
Published: (2014)
by: Stueber, Thomas J., et al.
Published: (2014)
Fuel-flexible gas turbine combustor flametube facility /
by: Little, James E.
Published: (2004)
by: Little, James E.
Published: (2004)
Cooling of rocket thrust chambers with liquid oxygen /
by: Armstrong, Elizabeth S.
Published: (1990)
by: Armstrong, Elizabeth S.
Published: (1990)
Integrated high payoff rocket propulsion technology (IHPRPT) SiC recession model /
by: Opila, E. (Elizabeth)
Published: (2009)
by: Opila, E. (Elizabeth)
Published: (2009)
Experimental clean combustor program : phase II : final report /
by: Gleason, C. C.
Published: (1976)
by: Gleason, C. C.
Published: (1976)
Optical and probe determination of soot concentrations in a model gas turbine combustor /
by: Eckerle, Wayne Alan
Published: (1986)
by: Eckerle, Wayne Alan
Published: (1986)
HBCUs/OMUs Research Conference agenda and abstracts : proceedings of a conference held at Ohio Aerospace Institute and sponsored by NASA Glenn Research Center, Cleveland, Ohio, April 17-18, 2002 /
Published: (2003)
Published: (2003)
Recent improvements to the Acoustical Testing Laboratory at the NASA Glenn Research Center /
by: Podboy, Devin M.
Published: (2014)
by: Podboy, Devin M.
Published: (2014)
Development status of a three-dimensional electron fluid model for hall thruster plume simulations /
by: Choi, Maria, et al.
Published: (2018)
by: Choi, Maria, et al.
Published: (2018)
Active combustion control for aircraft gas-turbine engines : experimental results for an advanced, low-emissions combustor prototype /
Published: (2012)
Published: (2012)