Results 41 to 50 of about 6,631,530 (188)

Procedures for the Safe Operation of Helicopters in an Energized Wire Environment

open access: yesSafety & Defense
This paper describes procedures for the safe operation of helicopters in an energized wire environment. The procedures are designed to respect the appropriate minimum distances that must be maintained between the extremities of the helicopter and ...
Eugeniusz Piechoczek, George Gela
doaj   +1 more source

Drag Characteristics and Reduction Test for Hub of Coaxial-rotor Helicopter

open access: yesHangkong gongcheng jinzhan, 2020
The drag of coaxial helicopter hub accounts is more than 50% of the total helicopter's waste drag, so it is necessary to research the drag characteristics and reduction design of the hub. Wind tunnel test is carried out for a coaxial helicopter hub model,
LONG Haibin, WU Yuping
doaj   +1 more source

ON THE QUESTION OF SAFETY OPERATION OF A HELICOPTER AFTER CARGO DISCHARGE FROM EXTERNAL SLING

open access: yesНаучный вестник МГТУ ГА, 2018
When helicopters fly with suspended load, there may be a need for a load drop. This can be associated with both the abnormal situations in flight and with a regular load drop to a predetermined area.
R. V. Volobuev, V. V. Efimov
doaj   +1 more source

Item - Test Alternate Title

open access: yes
Item - Test Description ...
Item - Test Creator 1   +2 more
core   +1 more source

Simulation of Backstepping-based Nonlinear Control for Quadrotor Helicopter

open access: yesApplications of Modelling and Simulation, 2018
The control of quadrotor helicopter in a hover condition has always been a great challenge for control engineers and researchers. Various algorithms have been developed to control this type of helicopter due to its high nonlinearities.
M. A. M. Basri   +2 more
doaj  

ASSESSING THE ADEQUACY OF MATHEMATICAL MODELS OF THE MI-8MTV HELICOPTER DYNAMICS IN TERMS OF CONTROLLABILITY

open access: yesНаучный вестник МГТУ ГА, 2016
The article considers the adequacy of a mathematical model of Mi-8MTV helicopter dynamics with an external load in terms of controllability, based on comparison of data obtained from computational experiments and flight testing. The results of evaluation
G. N. Babenko   +2 more
doaj  

A Numerical Method for Blast Shock Wave Analysis of Missile Launch from Aircraft

open access: yesInternational Journal of Aerospace Engineering, 2015
An efficient empirical approach was developed to accurately represent the blast shock wave loading resulting from the launch of a missile from a military aircraft to be used in numerical analyses.
Sebastian Heimbs   +2 more
doaj   +1 more source

Helicopter versus ground ambulance: review of national database for outcomes in survival in transferred trauma patients in the USA

open access: yesTrauma Surgery & Acute Care Open, 2019
Background Trauma care has improved substantially in the last decade. The emphasis of the Golden Hour in trauma care has encouraged the creation of faster transport and earlier prehospital intervention.
David Michaels   +3 more
doaj   +1 more source

Extracting Lateral Transfer Function of a Remotely Piloted Helicopter by System Identification Method Using 3-DOF Test Stand [PDF]

open access: yesInternational Journal of Advanced Design and Manufacturing Technology, 2011
At the beginning of this paper, design and manufacturing stages of the 3 degree of freedom test stand for a remotely piloted helicopter is described, in which the helicopter is able to rotate about its three primary accesses.
Hesamodin EbnodinHamidi   +2 more
doaj  

Performance and Vibration Analyses of Lift-Offset Helicopters

open access: yesInternational Journal of Aerospace Engineering, 2017
A validation study on the performance and vibration analyses of the XH-59A compound helicopter is conducted to establish techniques for the comprehensive analysis of lift-offset compound helicopters.
Jeong-In Go, Do-Hyung Kim, Jae-Sang Park
doaj   +1 more source

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