Results 121 to 130 of about 4,154,170 (239)

The DELTA MONSTER: An RPV designed to investigate the aerodynamics of a delta wing platform [PDF]

open access: yes
The mission requirements for the performance of aerodynamic tests on a delta wind planform posed some problems, these include aerodynamic interference; structural support; data acquisition and transmission instrumentation; aircraft stability and control;
Connolly, Kristen   +8 more
core   +1 more source

Noise source identification for ducted fans

open access: yes, 2006
Understanding combustion noise source mechanisms, designing efficient acoustic liners and optimising active control algorithms for noise reduction requires the identification of the frequency and modal content of the combustion noise contribution. Coherence-based noise source identification techniques have been developed which can be used to identify ...
openaire   +1 more source

NASA/industry advanced turboprop technology program [PDF]

open access: yes
Experimental and analytical effort shows that use of advanced turboprop (propfan) propulsion instead of conventional turbofans in the older narrow-body airline fleet could reduce fuel consumption for this type of aircraft by up to 50 percent.
Whitlow, John B., Jr.   +1 more
core   +1 more source

RTM fan ducts ordered

open access: yesReinforced Plastics, 2001
openaire   +1 more source

Rotating Rake Turbofan Duct Mode Measurement System [PDF]

open access: yes
An experimental measurement system was developed and implemented by the NASA Glenn Research Center in the 1990s to measure turbofan duct acoustic modes. The system is a continuously rotating radial microphone rake that is inserted into the duct.
Sutliff, Daniel L.
core   +1 more source

Ventilation approaches and radon control in Canadian houses. [PDF]

open access: yesFront Public Health
Gaskin J, Zhou LG, Li YE, Tardif P.
europepmc   +1 more source

Historical overview of V/STOL aircraft technology [PDF]

open access: yes
The requirements for satisfactory characteristics in several key technology areas are discussed and a review is made of various V/STOL aircraft for the purpose of assessing the success or failure of each design in meeting design requirements.
Anderson, S. B.
core   +1 more source

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