Results 11 to 20 of about 2,641 (299)
Modeling of a Novel Coaxial Ducted Fan Aerial Robot Combined with Corner Environment by Using Artificial Neural Network. [PDF]
Ai T, Xu B, Xiang C, Fan W, Zhang Y.
europepmc +3 more sources
The aerodynamic parameters of ducted fan micro aerial vehicles (MAVs) are difficult and expensive to precisely measure and are, therefore, not available in most cases. Furthermore, the actuator dynamics with risks of potentially destabilizing the overall
Shouzhao Sheng, Chenwu Sun
exaly +3 more sources
When developing counter-rotating fans for advanced aircraft engines with ducted blades (CRTF), it is very important to ensure high acoustic and aerodynamic characteristics. To provide investigations of aerodynamic and acoustic performance of the original
V. I. Mileshin +3 more
doaj +3 more sources
On dynamic characteristics and stability analysis of the ducted fan unmanned aerial vehicles
This article researches the improvement of dynamics stability of the ducted fan unmanned aerial vehicles by optimizing its mechanical–structure parameters.
Dong Tian
exaly +2 more sources
Development of an Ultralight with a Ducted Fan
This paper introduces the UL-39 project, an ultralight aircraft with a ducted fan, and some of the problems that have arisen in the course of its development. Several problems with the design of a non-traditional aircraft of this kind are mentioned, e.g.
Jiří Brabec, Martin Helmich
doaj +3 more sources
Matching fan and motor design parameters in electric ducted fans
Electric propulsion systems are gaining more research interest as a way to achieve zero-emission aviation. However, scaling up such systems for larger civil aircraft flying at higher flight speeds poses challenges. One major issue is aligning the performance of electric motors with the aerodynamic design of the fan. This paper discusses matching of the
Viacheslav A. Sedunin +2 more
openalex +2 more sources
A Study on Hover Performance of Ducted Fans for an Unmanned VTOL Aircraft
In this study, ground tests and numerical analysis were performed to verify the hover performance of the second ducted fan model designed by this research team.
Young Jae Choi +2 more
doaj +1 more source
Focusing on the aerodynamic characteristics of the blended wing body (BWB) aircraft with boundary layer ingestion(BLI) distributed propulsion system; the influences of propulsion system parameters under the condition of cruise and takeoff are studied ...
doaj +1 more source
Noise-Source Identification for Ducted Fan Systems [PDF]
Coherence-based source analysis techniques can be used to identify the contribution of combustion noise in the exhaust of a jet engine and to hence enable the design of noise-reduction devices. However, when the combustion noise propagates in a nonlinear fashion, the identified contribution using ordinary coherence methods will be inaccurate.
BENNETT, GARETH, FITZPATRICK, JOHN AIDAN
openaire +3 more sources
Effect of inlet distortion with crosswind on aircraft-engine intake aerodynamic performance
This paper describes an experimental study on inlet distortion in the flow ingested to an intake of a ducted fan. Recent high bypass ratio engines tend to shorten the nacelle length for better fuel consumption.
Hiroki NARUSE +7 more
doaj +1 more source

