16   Artículos

 
en línea
Antonio Chiariello, Carmine Carandente Tartaglia, Maurizio Arena, Vincenzo Quaranta, Giovanni Bruno, Marika Belardo and Martina Castaldo    
Revista: Aerospace    Formato: Electrónico

 
en línea
Yu-Been Lee and Jae-Sang Park    
This present study investigates the effect of blade tip configurations, such as the sweepback angle and anhedral angle, on the performance and hub vibratory loads for the lift-offset coaxial rotor of a 30,000-pound-class high-speed long-range utility hel... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Gianpietro Di Rito, Romain Kovel, Marco Nardeschi, Nicola Borgarelli and Benedetto Luciano    
The work deals with the model-based characterization of the failure transients of a fail-safe rotary EMA developed by Umbragroup (Italy) for the flap movables of the RACER helicopter-plane by Airbus Helicopters (France). Since the reference application r... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Ye Yuan, Douglas Thomson and David Anderson    
The tiltrotor has unique flight dynamics due to the aerodynamic interference characteristics. Multiple aerodynamics calculation approaches, such as the CFD method, are utilised to characterise this feature. The calculation process is usually time-consumi... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Chang Wang, Minqi Huang, Xianmin Peng, Guichuan Zhang, Min Tang and Haowen Wang    
The aerodynamic performance of a reduced-scale coaxial rigid rotor system in hover and steady forward flights was experimentally investigated to gain insights into the effect of interference between upper and lower rotors and the influences of the advanc... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Antonio Chiariello, Salvatore Orlando, Pasquale Vitale, Mauro Linari, Raffaele Longobardi and Luigi Di Palma    
In the framework of fast rotorcraft, smoothness and flushness of external aerodynamic surfaces present challenges for high-speed conditions, where aerodynamics is the driver of helicopter performance. For AIRBUS-RACER helicopter the main landing gear tra... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Khiem Van Truong    
To fulfill the objective of a predictive tool for rotorcraft, comprehensive analysis (CA) needs to be capable of providing both accurate and time-efficient predictions of rotor air loads and structural loads. The more recent methodology based on comprehe... ver más
Revista: Aerospace    Formato: Electrónico

« Anterior     Página: 1 de 1     Siguiente »