Zobrazeno 1 - 9
of 9
pro vyhledávání: '"Renita Sharon Monis"'
Autor:
null Renita Sharon Monis, null Asha Crasta, null Sher Afghan Khan, null Parvathy Rajendran, null Erwin Sulaeman
Publikováno v:
Journal of Advanced Research in Fluid Mechanics and Thermal Sciences. 92:1-8
Correlation investigation of quasi-steady and unsteady damping derivatives of delta wing is analyzed and contemplated, with leading edges bent in the current paper. The current paper realizes that the quasi-steady damping derivative considers only th
Publikováno v:
International Journal of Mechanical and Production Engineering Research and Development. 9:361-374
This paper presents the results of an analytical study to account the effect of the sweep angle of a delta wing whose leading edges are curved on roll damping derivative at various angles of attack and the amplitude of the full sine waves. In the pre
Autor:
Hamid Fardi, Z. D. Kovziridze, N. S. Nizharadze, G. Tabatadze, M. Mshvildadze, E. Nikoleishvili, Z. Mestvirishvili, Chávez-Sandoval Blanca Estela, A. Ibáñez-Hernández Miguel Angel, García-Franco Francisco, Galindo-Pérez Ezel Jacome, Abrica González Paulina, Martínez-Jiménez Anatolio, Balderas López José Abraham, Binu Sharma, S. K. Rahman, Panagis G. Papadopoulos, Christopher G. Koutitas, Panos P. Lazaridis, Larbi Hamiche, Salah Saad, Leila Merabet, Fares Zaamouche, Lizhi Zhang, Fan Li, Bo Sun, Chenghui Zhang, Aws Zuhair Sameen, Rosmina Jaafar, Mohammed Hasan Alwan, Jerzy Ratajski, Roman Olik, Tomasz Suszko, Jerzy Dobrodziej, Jerzy Michalski, Renita Sharon Monis, Asha Crasta, Sher Afghan Khan
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::63578a8d3518a8d6122cc4ea4d3f2afc
https://doi.org/10.9734/bpi/rder/v5
https://doi.org/10.9734/bpi/rder/v5
Publikováno v:
IOSR Journal of Mechanical and Civil Engineering. 16:97-104
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. Fr
Publikováno v:
IOSR Journal of Mechanical and Civil Engineering. 16:74-78
The aim of present study is to obtain mathematical expressions for surface pressure and its derivative with respect to Piston Mach number for an oscillating cone. The effects of Mach number and it’s geometry on Pressure and its derivative with resp
Publikováno v:
IOSR Journal of Mechanical and Civil Engineering. 16:29-36
The emphasis of this paper is to examine the variation of damping derivative with incidence angle and Mach number with varying pivot position. The damping derivative decreases with Mach number and increases with the incidence angle. It is also seen t
Publikováno v:
IOP Conference Series: Materials Science and Engineering. 370:012059
In this paper the expressions for stiffness and Damping derivatives are obtained in a closed form for perfect gas where the flow is quasi-steady and axi-axisymmetric, and the nose semi angle of the cone is such that the Mach number behind the shock .
Publikováno v:
IOP Conference Series: Materials Science and Engineering. 370:012061
Stability derivatives in Newtonian limit for an oscillating cone are obtained. Stiffness derivative decreases with pivot position for the entire range of cone angles. For cone angles in the range 20 to 30 degrees there is substantial increase in the
Publikováno v:
IOP Conference Series: Materials Science & Engineering; Jun2018, Vol. 370 Issue 1, p1-1, 1p