Incoming Resources
- Burner rig with an unattached duct for evaluating the erosion resistance of thermal barrier coatings, Robert A. Miller, Maria A. Kuczmarski, and Dongming Zhu
- Hybrid wing body shielding studies using an ultrasonic configurable fan artificial noise source generating typical turbofan modes, Daniel L. Sutliff and Clifford A. Brown, Bruce E. Walker
- Active noise control of low speed fan rotor-stator modes, Daniel L. Sutliff [and three others]
- Preconditioning the Helmholtz equation for rigid ducts, Kenneth J. Baumeister, Kevin L. Kreider
- Calculation of turbulence-driven secondary motion in ducts with arbitrary cross section, A.O. Demuren
- Validation of the predicted circumferential and radial mode sound power levels in the inlet and exhaust ducts of a fan ingesting distorted inflow, L. Danielle Koch
- High Reynolds number investigation of a flush-mounted, S-duct inlet with large amounts of boundary layer ingestion, Bobby L. Berrier, Melissa B. Carter, and Brian G. Allan
- A mode propagation database suitable for code validation utilizing the NASA Glenn advanced noise control fan and artificial sources, Daniel L. Sutliff
- The effects of acoustic treatment on pressure disturbances from a supersonic jet in a circular duct, Milo D. Dahl
- Parametric study of electromagnetic waves propagating in absorbing curved S ducts, Kenneth J. Baumeister