Tek-Tips is the largest IT community on the Internet today!
Members share and learn making Tek-Tips Forums the best source of peer-reviewed technical information on the Internet!
-
Congratulations TugboatEng on being selected by the Eng-Tips community for having the most helpful posts in the forums last week. Way to Go!
Recent content by Fajer
-
Landing Gear
ours is oleo pneumatic type this is modeled as mass spring damper system the landing gear system is a tricycle type.- Fajer
- Post #8
- Forum: Aircraft engineering
-
Landing Gear
5126 is the mass and it should bounce because its landing on a aircraft carrier. we have to assume the time thanks- Fajer
- Post #5
- Forum: Aircraft engineering
-
Landing Gear
the maximum deflection has been provided which = 0.3 m (Value Assumed ) For lynx 300 Helicpter Mass of the helicopter = 5126 Kg sink speed = 0.5m k= F/x = 5126/0.3 = 167620.2 N/m Need to find out damping ratio and Damping Coeficient at which the helicopter will have a deflection of 0.3 m- Fajer
- Post #3
- Forum: Aircraft engineering
-
Landing Gear
how to calculate the landing gear damping coefficient and stiffness for a non linear Spring type. I have only the mass of helicopter = 5126 Kg and initial velocity of 0.5m/s . Can anybody help please thanks- Fajer
- Thread
- Replies: 10
- Forum: Aircraft engineering
