Results 31 to 40 of about 12,334 (255)

Helicopter main rotor blade injury to the head with survival [PDF]

open access: yesJournal of the Royal Army Medical Corps, 1997
A case of soldier surviving a major helicopter rotor blade injury occurring in daylight is described and the limited literature on the subject is discussed.
J R, Gibbons   +3 more
openaire   +2 more sources

Helicopter Safe Landing Trajectory after Main Rotor Actuator Failures

open access: yesApplied Sciences, 2020
Main rotor actuator failure leads to catastrophic accidents for single main rotor helicopters. This paper focuses on safe landing trajectories after an actuator is locked in place by the remaining actuators, without introducing other control inputs.
Yunjie Wang   +3 more
doaj   +1 more source

Exploring the Detached-Eddy Simulation for Main Rotor Flows [PDF]

open access: yesRussian Aeronautics, 2018
This paper applies the Detached-Eddy Simulation (DES) method to resolve a larger part of the flow spectrum around rotor blades in hover and forward flight. A comparison between DES and Unsteady Reynolds–Averaged Navier–Stokes simulation was carried out for the case of a forward flying rotor suggesting that DES has great potential for rotor applications.
Dehaeze, F.   +4 more
openaire   +1 more source

Thrust pulsation of coaxial main rotor, caused by the blades relative position

open access: yesНаучный вестник МГТУ ГА, 2020
The influence of reciprocal position of the upper rotor blades in respect to the lower rotor blades is characteristic for coaxial main rotor. It is established that the initial azimuth of the blade, for example, of the upper rotor’s which does not ...
B. S. Kritsky   +3 more
doaj   +1 more source

Design of Composite Gyrocopter Main Rotor Blade Involving Rib and Spar Elements [PDF]

open access: yesJournal of Engineering, Project, and Production Management, 2019
Gyrocopter or gyroplane is a type of rotorcraft that uses an unpowered main rotor in free autorotation to develop lift. Gyrocopter rotor blades have smaller cord length and longer span compared to helicopters blades.
Yonas Mitik Degu, Derbew Alebel
doaj   +1 more source

Current Status and Challenges in Data Collection for Aerospace Coatings Deposited by Plasma Spraying

open access: yesAdvanced Engineering Materials, EarlyView.
An innovative approach has been integrated into the GRENAT project to optimize plasma spraying and coating performance. Raw materials are accelerated and melted in the plasma generated by torches, creating coatings. Monitoring sensors collect process data which are combined with ex situ characterization data.
Lila Randriamananjara   +8 more
wiley   +1 more source

D4.2 Preliminary Design (X-ROTOR) [PDF]

open access: yes, 2022
This document provides an overview of a first, feasible design for the X-ROTOR wind turbine, with particular focus on the jacket support structure.
Muskulus, Michael   +2 more
core   +1 more source

Optimization of the Production of Rubber Compounds Using Mathematical Models

open access: yesAdvanced Engineering Materials, EarlyView.
Rubber compounds were mixed in a batch internal mixer, and symbolic regression was used to derive mathematical models linking recipe and process parameters to ram path, torque, and mixing quality (incorporation, dispersion, distribution). Subsequent optimization with evolutionary algorithms identified operating conditions that reduce specific energy ...
Anke Bardehle   +7 more
wiley   +1 more source

Myrcene‐Based Tailored Co‐Polymers as Active Pharmaceutical Excipients: Bio‐Based Solutions for Mucoadhesive Excipients

open access: yesAdvanced Functional Materials, EarlyView.
Mucoadhesive amphiphilic block and statistical copolymers were synthesized via Reversible Addition–Fragmentation Chain Transfer polymerization from bio‐sourced myrcene and polyethylene glycol methacrylate. The resulting polymers exhibit narrow molar‐mass distributions, high regioselectivity, well‐defined microstructures, and tend to self‐assemble into ...
David Gintsburg   +9 more
wiley   +1 more source

Failure of a Helicopter Main Rotor Blade

open access: yesProcedia Materials Science, 2014
AbstractA military helicopter crash was investigated. The aircraft was flying at cruise speed in clear sky at 1000 feet over a flat area. The crew suddenly lost the control of the helicopter that crashed in the immediately causing fatal injuries to the whole crew.
Amura, Mikael   +4 more
openaire   +2 more sources

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