Add to ORKGThis note presents a preliminary analysis of the different solutions for the HF chopper for EURISOL post-accelerato
Tire de : 48th American Helicopter Society Forum, Washington DC (USA), June 3-5, 1992SIGLEAvailable ...
The aerodynamic design of rotor blades is challenging, and is crucial for the development of helicop...
Communication to : ECCOMAS 2000, Barcelona (Spain), September 11-14, 2000Available from INIST (FR), ...
The present document describes the thermal and the stress analysis of the final design of the EURISO...
Following a comparative study on shape morphing and adaptive systems to improve rotorcraft efficienc...
The symbol of the Hessian for an aeroelastic optimization model problem is analyzed
Combat helicopters frequently operate in the part of Planetary Boundary Layer (PBL) characterised by...
In the helicopter, the main rotor blade is mostly influenced by the aerodynamic forces and centrifug...
This work is the preliminary part of a research program which is aimed at finding some new methods a...
Communication to : American helicopter society - AHS, Forum 53, Virginia Beach (USA), April 29 - May...
SIGLECopy held by FIZ Karlsruhe; available from UB/TIB Hannover / FIZ - Fachinformationszzentrum Kar...
Also publ. as RAE-TM-AERO--1154Available from British Library Document Supply Centre- DSC:2265.63F(B...
Abstract: Aerodynamic characteristics of a 5-seater helicopter with different rotor configuration (i...
An aeroelastic analysis based on finite elements in space and time is used to model the helicopter r...
Helicopter flight dynamic, rotor aerodynamic and dynamic analyses activities have been a great dispu...
Tire de : 48th American Helicopter Society Forum, Washington DC (USA), June 3-5, 1992SIGLEAvailable ...
The aerodynamic design of rotor blades is challenging, and is crucial for the development of helicop...
Communication to : ECCOMAS 2000, Barcelona (Spain), September 11-14, 2000Available from INIST (FR), ...
The present document describes the thermal and the stress analysis of the final design of the EURISO...
Following a comparative study on shape morphing and adaptive systems to improve rotorcraft efficienc...
The symbol of the Hessian for an aeroelastic optimization model problem is analyzed
Combat helicopters frequently operate in the part of Planetary Boundary Layer (PBL) characterised by...
In the helicopter, the main rotor blade is mostly influenced by the aerodynamic forces and centrifug...
This work is the preliminary part of a research program which is aimed at finding some new methods a...
Communication to : American helicopter society - AHS, Forum 53, Virginia Beach (USA), April 29 - May...
SIGLECopy held by FIZ Karlsruhe; available from UB/TIB Hannover / FIZ - Fachinformationszzentrum Kar...
Also publ. as RAE-TM-AERO--1154Available from British Library Document Supply Centre- DSC:2265.63F(B...
Abstract: Aerodynamic characteristics of a 5-seater helicopter with different rotor configuration (i...
An aeroelastic analysis based on finite elements in space and time is used to model the helicopter r...
Helicopter flight dynamic, rotor aerodynamic and dynamic analyses activities have been a great dispu...
Tire de : 48th American Helicopter Society Forum, Washington DC (USA), June 3-5, 1992SIGLEAvailable ...
The aerodynamic design of rotor blades is challenging, and is crucial for the development of helicop...
Communication to : ECCOMAS 2000, Barcelona (Spain), September 11-14, 2000Available from INIST (FR), ...