z-logo
open-access-imgOpen Access
UAS Propeller/Rotor Sound Pressure Level Reduction Through Leading Edge Modification
Author(s) -
Mark N. Callender
Publication year - 2017
Publication title -
journal of applied mechanical engineering
Language(s) - English
Resource type - Journals
ISSN - 2168-9873
DOI - 10.4172/2168-9873.1000254
Subject(s) - propeller , rotor (electric) , reduction (mathematics) , enhanced data rates for gsm evolution , computer science , sound (geography) , sound pressure , acoustics , propulsor , engineering , mechanical engineering , marine engineering , physics , artificial intelligence , mathematics , geometry

The content you want is available to Zendy users.

Already have an account? Click here to sign in.
Having issues? You can contact us here