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  • 1
    facet.materialart.
    Unknown
    In:  Other Sources
    Publication Date: 2011-08-16
    Description: Discussion of the experimental Quiet Engine developed under the NASA program to reduce jet aircraft noise levels. The current status of the program is given as follows: Aerodynamic evaluation of the three fans is complete and their acoustic evaluation is partially complete. Tests of fan casing boundary-layer section and of serrated leading edges on the half-scale B fan are complete and are underway on the half-scale C fan. Tests of the first engine with the A fan began in August 1971.
    Keywords: PROPULSION SYSTEMS
    Type: Interavia; 26; Dec. 197
    Format: text
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  • 2
    facet.materialart.
    Unknown
    In:  Other Sources
    Publication Date: 2019-07-27
    Description: The NASA Quiet Engine Program will incorporate all available noise-reduction technology into a propulsion system suitable for subsonic civil transport aircraft. Full-scale experimental hardware is being built and tested primarily for noise performance. The program is in process, and component tests to date indicate that it is possible to achieve or exceed noise reduction objectives of 15-20 PNdB below the levels of 707/DC-8 long-range transport aircraft.
    Keywords: PROPULSION SYSTEMS
    Type: SAE PAPER 710774 , Society of Automotive Engineers, National Aeronautic and Space Engineering and Manufacturing Meeting; Sept. 28-30, 1971; Los Angeles, CA
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  • 3
    facet.materialart.
    Unknown
    In:  CASI
    Publication Date: 2019-06-27
    Description: Application of noise reduction technology to design of propulsion system for subsonic civil transport aircraft
    Keywords: PROPULSION SYSTEMS
    Type: NASA-TM-X-67884
    Format: application/pdf
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  • 4
    facet.materialart.
    Unknown
    In:  Other Sources
    Publication Date: 2019-07-13
    Description: Low noise subsonic commercial aircraft engine type and cycle selection
    Keywords: PROPULSION SYSTEMS
    Type: ASME PAPER 68-GT-61 , GAS TURBINE CONFERENCE AND PRODUCTS SHOW; Mar 17, 1968 - Mar 21, 1968; WASHINGTON, DC
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  • 5
    Publication Date: 2019-07-13
    Description: Design and specifications for low-noise output turbofan engine for long-range subsonic transport aircraft
    Keywords: PROPULSION SYSTEMS
    Type: NASA-TM-X-52640 , SYMP. ON MACHINERY NOISE; Nov 16, 1969 - Nov 21, 1969; LOS ANGELES
    Format: application/pdf
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  • 6
    facet.materialart.
    Unknown
    In:  CASI
    Publication Date: 2019-07-13
    Description: Initial studies on the design and testing of the quiet engine are described. The principal noise sources considered in the engine selection were the fan machinery noise and the fan and core jet noise. Nacelle acoustic linings are also mentioned. Fan and engine tests are discussed briefly and results indicate that it is possible to achieve or exceed noise reduction objectives of 15 to 20 PNdb below the levels of 707/DC-8 long-range transport aircraft.
    Keywords: PROPULSION SYSTEMS
    Type: NASA-TM-X-67988 , E-6729 , Ann. Intern. Gas Turbine Meeting; Mar 26, 1972 - Mar 30, 1972; San Francisco
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  • 7
    facet.materialart.
    Unknown
    In:  Other Sources
    Publication Date: 2019-08-13
    Description: NASA research and development work on the noise of aircraft engines suitable for use on conventional take-off and landing subsonic cruise airplanes is reviewed. The work discussed was part of the NASA Quiet Engine program. Salient results in the areas of fan, jet and complete propulsion system noise are presented and briefly discussed.
    Keywords: PROPULSION SYSTEMS
    Type: ICAS PAPER 72-48 , International Council of the Aeronautical Sciences, Congress; Aug. 28, 1972-Sept. 2, 1972; Amsterdam; Netherlands
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  • 8
    facet.materialart.
    Unknown
    In:  Other Sources
    Publication Date: 2019-08-13
    Description: Establishing the technology base for building a strong viable space program is a complex systems problem which demands continuous attention with full recognition of the dynamic state of the environment in which we operate. In the present paper, an attempt is made to outline, in a condensed form, NASA's approach to selecting those technologies which deserve to be pursued and ensuring that the probability of selecting the right technologies is maximized.
    Keywords: ASTRONAUTICS (GENERAL)
    Type: AAS PAPER 79-052 , American Astronautical Society, Goddard Memorial Symposium; Mar 28, 1979 - Mar 30, 1979; Washington, DC
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  • 9
    Publication Date: 2019-07-13
    Description: Design specifications for low noise turbofan engine used on long range subsonic transport aircraft
    Keywords: PROPULSION SYSTEMS
    Type: ASME PAPER 69-WA/G-7 , AMERICAN SOCIETY OF MECHANICAL ENGINEERS, WINTER ANNUAL MEETING; Nov 16, 1969 - Nov 20, 1969; LOS ANGELES, CA
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  • 10
    facet.materialart.
    Unknown
    In:  Other Sources
    Publication Date: 2019-07-13
    Description: The NASA quiet engine program will incorporate all available noise-reduction technology into a propulsion system suitable for subsonic civil transport aircraft. Full-scale experimental hardware is being built and tested primarily for noise performance. The program is in process, and component and engine tests to date indicate that it is possible to achieve or exceed noise reduction objectives of 15-20 PNdB below the levels of 707/DC-8 long-range transport aircraft.
    Keywords: PROPULSION SYSTEMS
    Type: ASME PAPER 72-GT-96 , American Society of Mechanical Engineers, Gas Turbine and Fluids Engineering Conference and Products Show; Mar 26, 1972 - Mar 30, 1972; San Francisco, CA
    Format: text
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