Model helicopter rotor high-speed impulsive noise : measured acoustics and blade pressures /

Bibliographic Details

Corporate Authors:	Ames Research Center, United States. Army Aviation Research and Development Command
Other Authors:	Boxwell, D. A.
Format:	Government Document Book
Language:	English
Published:	Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, [1983]
Series:	NASA technical memorandum ; 85850. AVARADCOM technical report ; 83-A-14.
Subjects:	Rotors (Helicopters) Impulses. Noise measurement. Propeller blades. Rotary wings.
Online Access:	https://purl.fdlp.gov/GPO/LPS89480