Turbofans
Resource Information
The concept Turbofans represents the subject, aboutness, idea or notion of resources found in University of Missouri-St. Louis Libraries.
The Resource
Turbofans
Resource Information
The concept Turbofans represents the subject, aboutness, idea or notion of resources found in University of Missouri-St. Louis Libraries.
- Label
- Turbofans
- Source
- nasat
33 Items that share the Concept Turbofans
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- Ultra-efficient engine diameter study
- Acoustic directivity and insertion loss measurements of advanced liners installed in the inlet of the DGEN aeropropulsion research turbofan
- Acoustic performance of novel fan noise reduction technologies for a high bypass model turbofan at simulated flight conditions
- Acoustic scattering by three-dimensional stators and rotors using the SOURCE3D code
- Acoustic testing of a high-tip-speed fan with bypass-duct liners--overview
- Advanced low-noise research fan stage design
- Azimuthal patterns of the radiated sound field from a turbofan model
- Boeing 18-inch fan rig broadband noise test
- Calculated performance of the NASA Lewis icing research tunnel
- Design of a low speed fan stage for noise suppression
- Effects of inlet distortion on aeromechanical stability of a forward-swept high-speed fan
- Energy efficient engine component development & integration program : semiannual report no. 7, April 1, 1981 - September 30, 1981
- Energy efficient engine low pressure subsystem flow analysis
- Energy efficient engine low pressure subsystem flow analysis
- Estimating engine airflow in gas-turbine powered aircraft with clean and distorted inlet flows
- Fission surface power technology development status
- Flutter analysis of a transonic fan
- Flutter analysis of a transonic fan
- Investigation of exoskeletal engine propulsion system concept
- Low noise research fan stage design
- Noise generation by fans with supersonic tip speeds
- Perceived noise analysis for offset jets applied to commercial supersonic aircraft
- Performance and weight estimates for an advanced open rotor engine
- Quiet High Speed Fan II (QHSF II) : final report
- Quiet high-speed fan
- Results of an advanced fan stage operating over a wide range of speed and bypass ratio
- Rotating rake turbofan duct mode measurement system
- Semi-empirical modeling and prediction of direct combustor noise
- Static performance of six innovative thrust reverser concepts for subsonic transport applications : summary of the NASA Langley Innovative Thrust Reverser Test Program
- Static performance of six innovative thrust reverser concepts for subsonic transport applications : summary of the NASA Langley Innovative Thrust Reverser Test Program
- The aerodynamic performance of an over-the-rotor liner with circumferential grooves on a high bypass ratio turbofan rotor
- Transfer-function determination for infinite-tube-probe pressure transducers with application to turbofan core/combustor noise
- Turbofan noise propagation and radiation at high frequencies
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<div class="citation" vocab="http://schema.org/"><i class="fa fa-external-link-square fa-fw"></i> Data from <span resource="http://link.umsl.edu/resource/HnibjcTx9dM/" typeof="CategoryCode http://bibfra.me/vocab/lite/Concept"><span property="name http://bibfra.me/vocab/lite/label"><a href="http://link.umsl.edu/resource/HnibjcTx9dM/">Turbofans</a></span> - <span property="potentialAction" typeOf="OrganizeAction"><span property="agent" typeof="LibrarySystem http://library.link/vocab/LibrarySystem" resource="http://link.umsl.edu/"><span property="name http://bibfra.me/vocab/lite/label"><a property="url" href="http://link.umsl.edu/">University of Missouri-St. Louis Libraries</a></span></span></span></span></div>
