Jet noise physics and modeling using first-principles simulationsFormat: [microform] /
Author: Freund, Jonathan B.
Publisher: [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ;
Date: 2003] This title can be found in 1 Iowa libraries.
A 3-D CE/SE Navier-Stokes solver with unstructured hexahedral grid for computation of near field jet screech noiseFormat: [microform] /
Author: Loh, Ching Y.
Publisher: [Cleveland, Ohio : NASA Glenn Research Center,
Date: 2003] This title can be found in 1 Iowa libraries.
Acoustic and laser doppler anemometer results for confluent, 22-lobed, and unique-lobed mixer exhaust systems for subsonic jet noise reductionFormat: [microform] /
Publisher: [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ;
Date: [2002] This title can be found in 1 Iowa libraries.
Acoustic and laser doppler anemometer results for confluent and 120-lobed E3 mixer exhaust systems for subsonic jet noise reductionFormat: [microform] /
Publisher: [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ;
Date: [2002] This title can be found in 1 Iowa libraries.
Large Engine Technology (LET) task XXXVII low-bypass ratio mixed turbofan engine subsonic jet noise reduction program test reportFormat: [microform] /
Author: Hauser, Joseph R.
Publisher: [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ;
Date: [2001] This title can be found in 1 Iowa libraries.
Recent developments in U.S. engine noise reduction researchFormat: [microform] /
Author: Bridges, James
Publisher: Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center ;
Date: [2001] This title can be found in 1 Iowa libraries.
Simulation of supersonic jet noise with the adaptation of overflow CFD code and Kirchhoff surface integralFormat: [microform] /
Author: Kandula, Max.
Publisher: Kennedy Space Center, Fla. : National Aeronautics and Space Administration, John F. Kennedy Space Center ;
Date: 2001] This title can be found in 1 Iowa libraries.
Acoustic and aerothermal performance test of the axisymmetric coannular ejector nozzleFormat: [microform] /
Author: Herkes, William.
Publisher: [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ;
Date: 2000- This title can be found in 1 Iowa libraries.
Separate flow nozzle test status meeting proceedings of a conference held at and sponsored by NASA Glenn Research Center, Cleveland, Ohio, September 9-10, 1997 /Format: [microform] :
Publisher: [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ;
Date: [2000] This title can be found in 1 Iowa libraries.
AST critical propulsion and noise reduction technologies for future commercial subsonic engines separate-flow exhaust system noise reduction concept evaluation /Format: [microform] :
Publisher: [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ;
Date: [2000] This title can be found in 1 Iowa libraries.
Noise certification predictions for FJX-2-powered aircraft using analytic methodsFormat: [microform] /
Author: Berton, Jeffrey J.
Publisher: [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ;
Date: 1999] This title can be found in 2 Iowa libraries.
Survey of turbulence models for the computation of turbulent jet flow and noiseFormat: [microform] /
Author: Nallasamy, M.
Publisher: [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ;
Date: 1999] This title can be found in 2 Iowa libraries.
Noise computation of a shock-containing supersonic axisymmetric jet by the CE/SE methodFormat: [microform] /
Publisher: [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ;
Date: 1999] This title can be found in 1 Iowa libraries.
XV-15 low-noise terminal area operations testing /Author: Edwards, B. D.
Publisher: Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center,
Date: [1998] This title can be found in 1 Iowa libraries.
Benefits of swept and leaned stators for fan noise reductionFormat: [microform] /
Publisher: [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ;
Date: 1998] This title can be found in 1 Iowa libraries.
Noise reduction with lobed mixers nozzle-length and free-jet speed effects /Format: [microform] :
Publisher: [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ;
Date: [1997] This title can be found in 2 Iowa libraries.
Large scale turbulent structures in supersonic jetsFormat: [microform] /
Author: Rao, Ram Mohan.
Publisher: Minneapolis, MN : Dept. of Aerospace Engineering and Mechanics, University of Minnesota ;
Date: 1997] This title can be found in 2 Iowa libraries.
Analysis of Particle Image Velocimetry (PIV) data for application to subsonic jet noise studiesFormat: [microform] /
Author: Blackshire, James L.
Publisher: Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ;
Date: 1997] This title can be found in 2 Iowa libraries.
Time correlations and the frequency spectrum of sound radiated by turbulent flowsFormat: [microform] /
Author: Rubinstein, Robert
Publisher: Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ;
Date: 1997] This title can be found in 2 Iowa libraries.
Ejector noise suppression with auxiliary jet injection under contract NAS3-27246 /Format: [microform] :
Author: Berman, Charles H.
Publisher: [Washington, DC : National Aeronautics and Space Administration ;
Date: 1997] This title can be found in 2 Iowa libraries.
This resource is supported by the Institute of Museum and Library Services under the provisions of the Library Services and Technology Act as administered by State Library of Iowa.