Development of a wind tunnel model testing for pure pitching motion /
Project paper (Bachelor of Mechanical Engineering (Aeronautical)) - Universiti Teknologi Malaysia, 1996
Main Author: | Iskandar Shah Ishak, 1973- |
---|---|
Format: | |
Published: |
Sekudai : UTM,
1996
|
Subjects: |
Similar Items
-
The design and development of a digital computer interfaces for the dynamic wind tunnel test rig /
by: 450143 Ong, Ming Wei
Published: (1998) -
Kajian angin lintang : pengujian terowong angin; The design and development of a two component force balance system for low speed wind tunnel; Development of a wind tunnel model testing for pure pitching motion; Computer graphic display of aircraft head up display (HUD); Performance of aerial sprayer / [mikrofilem]
by: Afifudden Mohamad Isa, et al.
Published: (1996) -
Model testing and simulation of a light aircraft design /
by: 429541 Shuhaimi Mansor
Published: (1998) -
Developement of a dynamic wind tunnel rig for aircraft pure pitching motion [UTM article journal]/
by: Shuhaimi Mansor -
Wind tunnel test on AS5045 airfoil using force balance /
by: Helizam Alinifiah, 1987-, et al.
Published: (2010)