Crasta, Asha and Shabana, Aysha and Monis, Renita and Khan, Sher Afghan (2016) Analysis of variation of stiffness derivative with Mach number and angle of attack for a supersonic flow. IOSR Journal of Mechanical & Civil Engineering, 12 (6). pp. 97-104. ISSN 2320-334x E-ISSN 2278-1684
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Abstract
In this paper unified supersonic theory is used to derive the expressions of Stiffness derivative of a wedge in Hypersonic flow. This paper demonstrates the effects of pivot position on the stffness derivative with Mach number and incidence angle. From the above discussion it is seen that behaviour of the stiffness derivative is the same for h = 0 to 0.4 and also for h = 0.8, 0.9, and 1.0. Due to the pivot position variations there is a significant variation of Stiffness derivative with Mach number and incidence angle.
Item Type: | Article (Journal) |
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Additional Information: | 7395/54287 |
Uncontrolled Keywords: | Incidence angle, stiffness derivative, supersonic flow, variation |
Subjects: | V Naval Science > V Naval Science (General) |
Kulliyyahs/Centres/Divisions/Institutes (Can select more than one option. Press CONTROL button): | Kulliyyah of Engineering > Department of Mechanical Engineering |
Depositing User: | Prof. Dr. Sher Afghan Khan |
Date Deposited: | 23 Jan 2017 09:55 |
Last Modified: | 31 Jan 2017 14:18 |
URI: | http://irep.iium.edu.my/id/eprint/54287 |
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