scholarly journals A proposed procedure for expressing the behavior of a full engine cycle by identifying its critical load timings

Author(s):  
Mihalache Marius Andrei ◽  
Nagit Gheorghe ◽  
Musca Gavril ◽  
Merticaru Vasile ◽  
Ripanu Marius Ionut
Keyword(s):  
2000 ◽  
Vol 33 (13) ◽  
pp. 4836-4841 ◽  
Author(s):  
P. Adriaensens ◽  
L. Storme ◽  
R. Carleer ◽  
D. Vanderzande ◽  
J. Gelan ◽  
...  

Author(s):  
Jia-Bin Sun ◽  
Xin-Sheng Xu ◽  
Chee-Wah Lim

AbstractIn this paper, the dynamic buckling of an elastic cylindrical shell subjected to an axial impact load is analyzed in Hamiltonian system. By employing a symplectic method, the traditional governing equations are transformed into Hamiltonian canonical equations in dual variables. In this system, the critical load and buckling mode are reduced to solving symplectic eigenvalues and eigensolutions respectively. The result shows that the critical load relates with boundary conditions, thickness of the shell and radial inertia force. And the corresponding buckling modes present some local shapes. Besides, the process of dynamic buckling is related to the stress wave, the critical load and buckling mode depend upon the impacted time. This paper gives analytically and numerically some new rules of the buckling problem, which is useful for designing shell structures.


2015 ◽  
Vol 94 ◽  
pp. 293-301 ◽  
Author(s):  
J. Awrejcewicz ◽  
A.V. Krysko ◽  
I.V. Papkova ◽  
I.Y. Vygodchikova ◽  
V.A. Krysko

1984 ◽  
Vol 21 (6) ◽  
pp. 269-272 ◽  
Author(s):  
K. E. Egorov ◽  
T. I. Finaeva
Keyword(s):  

2014 ◽  
Vol 20 (1) ◽  
pp. 53-79 ◽  
Author(s):  
Roger Fosdick ◽  
Pilade Foti ◽  
Aguinaldo Fraddosio ◽  
Salvatore Marzano ◽  
Mario Daniele Piccioni

1994 ◽  
Vol 356 ◽  
Author(s):  
V. A. C. Haanappel ◽  
H. D. van Corbach ◽  
T. Fransen ◽  
P. J. Gellings

AbstractAmorphous alumina films were deposited by metal-organic chemical vapour deposition (MOCVD) on stainless steel, type AISI 304. The MOCVD experiments were performed in nitrogen at low pressure (0.17 kPa (1.25 torr)).The effect of deposition temperature (200 − 380 °C), growth rate, film thickness, and post-deposition thermal treatment on the mechanical properties was studied. The experiments were performed with a scanning-scratch tester. The experiments are based on the estimation of the film adhesion to the substrate by determining a critical load, Lc: the load where the film starts to spall or to delaminate.The best mechanical properties were obtained with unannealed samples. After thermal annealing the critical load decreases. Regarding the unannealed samples, the critical load increased with increasing film thickness. The deposition temperature and the growth rate had no effect on the critical load.


Sign in / Sign up

Export Citation Format

Share Document