Feasibility study on improving of 5-seater helicopter forward flight speed
In this study, two 5-seater helicopters that are in the same FAR 27 category were chosen for the forward flight speed comparison. In order to improve the helicopter cruising speed, the main rotor blade of a helicopter that posses a lesser flight speed was modified through the usage of different numb...
Saved in:
Main Author: | Nik Mohd., Nik Ahmad Ridhwan |
---|---|
Format: | Thesis |
Language: | English |
Published: |
2006
|
Subjects: | |
Online Access: | http://eprints.utm.my/id/eprint/5565/1/NikAhmadRidhwanMFKM2006.pdf |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Similar Items
-
A computational simulation of rotor-fuselage flow interaction in hovering and forward flight
by: Ismail, Mohamad Hafiz
Published: (2007) -
The development of autopilot system for an unmanned aerial vehicle (UAV) helicopter model
by: Shamsudin, Syariful Syafiq
Published: (2007) -
Autorotation performance of unmanned aerial vehicle helicopter using rectangular and quadratic blades
by: Mat Ali, Mohamed Sukri
Published: (2007) -
Computational fluid dynamics of unsteady aerodynamic wake on helicopter main rotor-hub assembly
by: Othman, Nurain
Published: (2022) -
Performance prediction for high speed craft
by: Bero, Anuar
Published: (2009)