Results 101 to 110 of about 191,773 (209)

Psychoacoustic Test to Determine Sound Quality Metric Indicators of Rotorcraft Noise Annoyance [PDF]

open access: yes
Noise certification metrics such as Effective Perceived Noise Level and Sound Exposure Level are used to ensure that helicopters meet regulations, but these metrics may not be good indicators of annoyance since noise complaints against helicopters ...
Christian, Andrew   +2 more
core   +1 more source

Rotorcraft research testing in the National Full-Scale Aerodynamics Complex at NASA Ames Research Center [PDF]

open access: yes
The unique capabilities of the National Full-Scale Aerodynamics Complex (NFAC) for testing rotorcraft systems are described. The test facilities include the 40- by 80-Foot Wind Tunnel, the 80- by 120-Foot Wind Tunnel, and the Outdoor Aerodynamic Research
Johnson, W., Smith, C. A., Warmbrodt, W.
core   +1 more source

HELICOPTERS [PDF]

open access: yesAnesthesiology, 1971
openaire   +1 more source

Assessment of worm gearing for helicopter transmissions [PDF]

open access: yes
A high-efficiency hydrostatic worm gear drive for helicopter transmissions is assessed. The example given is for a large cargo helicopter with three 4000-kW engines and transmission reduction ratio of 110. Also contained are: an efficiency calculation, a
Chaiko, Lev
core   +1 more source

CFD-enabled sustainable design and manufacturing of cooling fan for unmanned helicopter. [PDF]

open access: yesSci Rep
Si L   +10 more
europepmc   +1 more source

Helicopter rotor trailing edge noise [PDF]

open access: yes
A two dimensional section of a helicopter main rotor blade was tested in an acoustic wind tunnel at close to full-scale Reynolds numbers to obtain boundary layer data and acoustic data for use in developing an acoustic scaling law and testing a first ...
Amier, R. K., Schlinker, R. H.
core   +1 more source

Effects of drop net and helicopter net-gun capture on movement, space use, and survival of white-tailed deer. [PDF]

open access: yesPLoS One
Stewart DG   +6 more
europepmc   +1 more source

Home - About - Disclaimer - Privacy