Results 91 to 100 of about 2,332 (184)

Flow visualization and flow field measurements of a 1/12 scale tilt rotor aircraft in hover [PDF]

open access: yes
The results are given of flow visualization studies and inflow velocity field measurements performed on a 1/12 scale model of the XV-15 tilt rotor aircraft in the hover mode.
Coffen, Charles D.   +3 more
core   +1 more source

Mode transition control of large-size tiltrotor aircraft

open access: yes
Tiltrotors are an aircraft concept with the ability to rotate their rotors freely, achieving vertical take-off and fast forward flight. The combination of helicopter and fixed-wing flight into one aircraft provides versatility in mission selection, yet challenges persist in their construction and control. Tiltrotor aircraft can operate in three primary
Kirst, George, Wang, Xinhua
openaire   +2 more sources

Quick trim modeling for tiltrotor aircraft in conversion mode

open access: yesJournal of Physics: Conference Series
Abstract The conversion mode in tiltrotor aircraft is of paramount importance and complexity, necessitating the trim results to ensure stable tilting using the trim model. Quick trim modeling is conducted for tiltrotor aircraft in conversion mode, focusing on the aerodynamics of the rotor using modified lift line theory.
Xincui Zhang   +3 more
openaire   +1 more source

Technology Assessment for Large Vertical-Lift Transport Tiltrotors [PDF]

open access: yes
The technical community has identified rotor efficiency as a critical enabling technology for large vertical-lift transport (LVLT) rotorcraft. The size and performance of LVLT aircraft will be far beyond current aircraft capabilities, enabling a ...
Germanowski, Peter J.   +2 more
core   +1 more source

Co-design Optimization of a Novel Multi-identity Drone Helicopter (MICOPTER). [PDF]

open access: yesJ Intell Robot Syst, 2022
Abedini A, Bataleblu AA, Roshanian J.
europepmc   +1 more source

Aerodynamic blade design with multi-objective optimization for a tiltrotor aircraft

open access: yesAircraft Engineering and Aerospace Technology, 2015
Purpose – The purpose of this paper is to present the aerodynamic blade design of a tiltwing aircraft with a multi-objective optimization procedure. The aerodynamic design of tiltrotor blades is a very challenging task in the project of this type of aircraft.
DROANDI, GIOVANNI, GIBERTINI, GIUSEPPE
openaire   +1 more source

Aerogels for Thermal Protection and Their Application in Aerospace. [PDF]

open access: yesGels, 2023
Jin R   +8 more
europepmc   +1 more source

Potential use of tiltrotor aircraft in Canadian aviation [PDF]

open access: yes
The aviation system in Canada is described as it relates to the potential applicability of tiltrotor technology. Commuter service in two corridors, the Vancouver-Victoria route on the west coast and the heavily traveled Montreal-Toronto corridor in ...
Alton, Larry, Gazdag, Denyse
core   +1 more source

Integration of Rotor Aerodynamic Optimization with the Conceptual Design of a Large Civil Tiltrotor [PDF]

open access: yes, 2010
Coupling of aeromechanics analysis with vehicle sizing is demonstrated with the CAMRAD II aeromechanics code and NDARC sizing code. The example is optimization of cruise tip speed with rotor/wing interference for the Large Civil Tiltrotor (LCTR2) concept
Acree, C. W., Jr.
core   +1 more source

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