Asad Raza (195111) <br/><br/>
Computational Modelling of Dynamic Stability Derivatives For Complete Aircraft Configuration Using Quasi Steady Frame Rotation 

 - Kamra:  Department of Aerospace Engineering,  2021. 
 - 68 p. 
<br/><br/><label>Subjects--Topical Terms: </label><br/>Department of Aerospace Engineering. (Thesis)
<br/><br/><label>Dewey Class. No.: </label>629.1  / ASA - MSAE