Development of a dynamic wind tunnel rig for aircraft pure pitching motion

This paper presents the design, fabrication and testing of a dynamic wind tunnel test rig that is used in conjunction with aircraft dynamics theory in estimating aerodynamics stability derivatives. The value of and can be obtained from free oscillation theory of pure pitching motion. The rig compris...

Πλήρης περιγραφή

Λεπτομέρειες βιβλιογραφικής εγγραφής
Κύριοι συγγραφείς: Mansor, Shuhaimi, Ishak, Iskandar Shah, Ong, Meng Wei, Fahrurazi, Istas
Μορφή: Άρθρο
Γλώσσα:English
Έκδοση: Faculty of Mechanical Engineering 2000
Θέματα:
Διαθέσιμο Online:http://eprints.utm.my/8314/1/ShuhaimiMansor2000_DevelopmentofaDynamicWind.pdf