Computational Evaluation of Aerodynamic Loading on Retractable Landing-Gears
Computational fluid dynamics is employed to evaluate the mean aerodynamic loading on the retractable landing-gears of a regional transport commercial aircraft. The mean turbulent flow around simplified landing-gear systems including doors is simulated by
Giuliano De Stefano +3 more
doaj +1 more source
Experimental Investigations on the Possibility to Apply the Corrugated Sheet Metal Used in the Past with Junkers Aircraft to Reduce Noise for Future European Aircraft. Other Noise Reduction Experiments for Future European Aircraft [PDF]
This paper shows that corrugated skin used in the past with Junkers aircraft to increase the fuselage and wing rigidity can lead to noise reduction for future European aircraft. If the pressure side of wing which is placed above the engine is corrugated,
Constantin SANDU +4 more
doaj +1 more source
The modern undercarriage system of a large aircraft normally requires the landing gear to be retractable. The nose landing gear, installed in the front of the fuselage, is retracted either forward or rearward.
Yong Liang +4 more
doaj +1 more source
Based on the technical platform of electrically actuated nose wheel steering systems, a new type of damping shimmy reduction technology is developed to break through the limitations of traditional hydraulic damping shimmy reduction methods, and an ...
Chenfei She +5 more
doaj +1 more source
Dynamics Simulation Research on Tricycle Landing Gear UAV During Taxiing and Take-off Phase
The UAV taxiing and take-off phase is a dangerous phase in the flight process, during which the force of UAV is very complex and the dynamic characteristics is different from that in the air.
Zhang Lin, Gong Xiying, Pang Junfeng
doaj +1 more source
Analysis of Carrier-Based Aircraft Catapult Launching Based on Variable Topology Dynamics
The catapult process of a carrier-based aircraft includes multiple links such as catapult tensioning, separation of the holding rod, dragging and running, separation of the catapult and drag shuttle, and free running. The connection relationships between
Hu Chen, Xingbo Fang, Hong Nie
doaj +1 more source
Material Replacement and Fatigue Analysis of Nose Landing Gear’s Shock Strut
Landing, take off are one of the most maneuvering occurring in aircraft. The landing gear is considered as a non-linear structure due to its complicate behavior during landing period large amount of impact forces transferred into nose gear and main ...
Nishanth P +5 more
semanticscholar +1 more source
Shimmy analysis of light weight aircraft nose wheel landing gear
This paper presents mathematical modeling and analysis of shimmy oscillations for a light weight airplane single wheel nose landing gear. Shimmy is a self-excited oscillation which occurs usually on the nose wheel landing gear assembly during ground maneuvers which is governed by the dynamic characteristics of the landing gear and tires.
V. Giridharan, S. Sivakumar
openaire +1 more source
Considering lateral bending and torsion coupling in shimmy analysis of the nose landing gear
This paper focuses on the shimmy damper performance of nose landing gear and aims to establish and amend a five-dimensional dynamic model of nose landing gear.
Peng Zhang +5 more
semanticscholar +1 more source
Lack of capture‐induced mortality of neonates associated with variation in handling protocols
We found that handling metrics (e.g., handling time, number of collectors, and age at capture) had limited or no influence on the survival of neonatal mule deer, desert bighorn sheep, and Rocky Mountain bighorn sheep within the first few days of life. Furthermore, we found that handled mule deer and Rocky Mountain bighorn neonates were recruited at a ...
Marcus E. Blum +24 more
wiley +1 more source

