Analytical models for rotor test module, strut, and balance frame dynamics in the 40- by 80-ft wind tunnel /
Saved in:
Main Author: | Johnson, Wayne, 1946- (Author) |
---|---|
Format: | Government Document Electronic eBook |
Language: | English |
Published: |
Moffett Field, California :
Ames Research Center, NASA, and Ames Directorate, USAAMRDL,
June 1976.
|
Series: | NASA technical memorandum ;
X-73153. |
Subjects: | |
Online Access: | CONNECT |
Similar Items
-
Acoustic measurements from a rotor blade-vortex interaction noise experiment in the German-Dutch wind tunnel (DNW) /
by: Martin, R. M. 1956-
Published: (1988) -
Performance and vibratory loads data from a wind-tunnel test of a model helicopter main-rotor blade with a paddle-type tip /
by: Yeager, William T.
Published: (1997) -
Two-dimensional wind tunnel.
Published: (1982) -
Wind-tunnel evaluation of the effect of blade nonstructural mass distribution on helicopter fixed-system loads /
by: Wilbur, Matthew L.
Published: (1998) -
Performance optimization of a rotor alone Nacelle for acoustic fan testing /
by: Cunningham, C. C., et al.
Published: (2000)