 | Aeronautical engineering |
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 | Generalised Model for Aircraft Vulnerability by Different Weapon Systems
Author : Singh, V.P.;Singh, Yuvraj
Source : Defence Science Journal ; Vol:50(1) ; 2000 ; pp 13-23
Subject : 629.7 Aeronautics;623.41 Weapon Systems
Keywords : Curvelinear triangles;Fused ammunition;Military aircrafts;Aeronautical engineering;Flight tests
Abstract : The authors earlier model for the vulnerability of aircraft where aircraft was considered as a combination of cylinder, cones and wedges has been extended to the case when structural data of aircraft as well as its vital parts are given in the form of three-dimensional curvilinear triangles. In the case of VT -fused ammunition, spherical normal distribution has been used to estimate the landing probability of the shell in a cylindrical vicinity region around the aircraft. Kill criteria of vital parts have been redefined. |
| | Diffusion Bonding Aeroengine Components
Author : Fitzaptrick, G.A.;Broughton, T.
Source : Defence Science Journal ; Vol:38(4) ; 1988 ; pp 477-486
Subject : 629.7 Aeronautics
Keywords : Diffusion bonding processes;Aeronautical engineering;Liquid phase diffusion bonding
Abstract : Abstract not available. |
| | Body measurement s in relation to cockpit design
Author : Iyer, P. V. Krishna;Bhattacharyya, M. N.
Source : Defence Science Journal ; Vol:16(1) ; 1966 ; pp 51-56
Subject : 629.7 Aeronautics
Keywords : Aeronautical engineering;Physical charactristics;Cockpits;Cockpit design
Abstract : The paper deals with the major conclusions arising from the statistical analysis of 22 body Measurements of 691 airmen. Besides the upper and lower 95 per rent confidence limits for these characters, the regression equations for (i) body a-eight on the measurement of abdomen, shoulder, elbow, seat maximum below hips and total height and (ii ) total height on knee height and thigh height, have also been given. |
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