Results 101 to 110 of about 310,977 (203)
Design of retractable mechanism of small airplane nose landing gear
Tato bakalářská práce se zabývá návrhem mechanismu zatahování příďového podvozku malého sportovního letounu. V práci je navrhnuta kinematika mechanismu zatahování příďového podvozku, rozbor zatížení a základní návrh konstrukčního řešení mechanismu.This ...
Paul Ondřej
core
To optimize and improve the nose landing gear shock absorber of a fixed-wing carrier-based aircraft, the cross-sectional area of the oil needle in the main oil orifice and the cross-sectional area of the oil return orifice shall be reconfigured. Firstly,
Wenlin Liu +4 more
doaj +1 more source
Main landing gear merupakan salah satu komponen paling penting pada pesawat terbang. Kegagalan komponen main landing gear akan mengakibatkan kerusakan yang parah pada struktur pesawat secara keseluruhan.
Sahril Afandi Sitompul +2 more
core
Physics-based aeroacoustic modelling of bluff-bodies
In this work physics-based modelling of bluff-body noise was performed with application to landing gear noise production. The landing gear is a primary contributor to airframe noise during approach.
Peers, Edward
core +1 more source
A Custom Genetic Algorithm Framework for Early-Stage Optimization of Electromechanical Actuators
This work presents a systematic methodology for the preliminary design and optimization of electromechanical actuators, aimed at minimizing overall mass and rotational inertia while satisfying torque and speed requirements.
Michelangelo Levati +5 more
doaj +1 more source
The Nose Landing Gear Design Of Light Aircraft
Tez (Yüksek Lisans) -- İstanbul Teknik Üniversitesi, Fen Bilimleri Enstitüsü, 1996Thesis (M.Sc.) -- İstanbul Technical University, Institute of Science and Technology, 1996Bu tez çalışması burun iniş takımı dizaynın sınıf I ve sınıf II metodlan ile ...
Gündoğdu, Ercan
core
A Multi-Step CNN-Based Estimation of Aircraft Landing Gear Angles. [PDF]
Li F, Wu Z, Li J, Lai Z, Zhao B, Min C.
europepmc +1 more source
Research on the Stability and Bifurcation Characteristics of a Landing Gear Shimming Dynamics System
A dynamic model is established to investigate the shimmy instability of a landing gear system, considering the influence of nonlinear damping. The stability criterion is utilized to determine the critical speed at which the landing gear system becomes ...
Shuang Ruan +4 more
doaj +1 more source
Conceptual design and optimization of a sustainable and environmentally friendly archetypal helicopter within the selection criteria and limitations. [PDF]
Gunaltili E +6 more
europepmc +1 more source
Innovative Photonic Sensors for Safety and Security, Part II: Aerospace and Submarine Applications. [PDF]
Cutolo A +30 more
europepmc +1 more source

