A compressible, high frequency numerical model of helicopter noise due to blade/vortex interaction
Thesis: M.S., Massachusetts Institute of Technology, Department of Aeronautics and Astronautics, 1980
Main Author: | Lima, Luiz Hamilton de Resende. |
---|---|
Other Authors: | Massachusetts Institute of Technology. Department of Aeronautics and Astronautics. |
Format: | Thesis |
Published: |
Massachusetts Institute of Technology
2025
|
Subjects: | |
Online Access: | https://hdl.handle.net/1721.1/158221 |
Similar Items
-
Receding horizon control of a 3 DOF helicopter using online estimation of aerodynamic parameters
by: Mehndiratta, Mohit, et al.
Published: (2020) -
Blade faults diagnosis in multi stage rotor system by means of wavelet analysis
by: Abdelrhman Ahmed, Ahmed Mohammed
Published: (2024) -
Short term distortion in dynamic noise-filters.
by: Wright, John Nelson.
Published: (2024) -
Magneto-optical studies in In[subscript 1-x]Ga[subscript x]As[subscript y]P[subscript 1-y] semiconducting alloys
by: Alavi, Kambiz.
Published: (2024) -
Magnetooptical studies of small-gap semiconductors : Hg₁₋ Cd Te and InSb
by: Weiler, Margaret Horton.
Published: (2024)