The design of the aeroplane is constantly changing but new designs are drawn with regard to increasing the efficiency of the machine. Already we have reached a stage at which, on account of "blacking out", the efficiency of the machine, under certain conditions at least, is greater than that of the pilot controlling it. This deficiency on the part of the pilot is due to the force of the acceleration acting on him during these manoeuvres. One cannot remove these forces but their effect can be rendered void by changing their direction of application. This, unfortunately involves revolution in the design of the aeroplane but it can be done. If, then, the future of the aeroplane is to advance, future designs of the aeroplane must be drawn with ...
In choosing the above title as the subject of a Thesis, I was impressed in my clinical work by the r...
The present research comprises: a. the development of an arithmetical trial and error method of find...
The downwash behind a wing may be computed from the system of vortices created by the wing and which...
The Thesis is divided primarily into three parts. In the first of these three parts is considered th...
Proper acoustic excitation of a single large-eddy break-up device can increase the resulting drag re...
Mainly as a result of the finding of the enquiry into the Whitehaven Colliery Explosion (1931), the ...
In part one the heredity of myopia,night-blindness and retinitis pigmentosa in association with othe...
Profile-drag coefficients published from tests in the N.A.C.A. variable-density tunnel (Technical Re...
The objective of this research is to increase the analytical capability of the existing TDK/BLM comp...
(a) That Pulmonary phthisis is an infectious disease and although hereditary predisposition has some...
This analysis computes for a predetermined airfoil and given Reynolds Number the course of the "disp...
Preliminary designs and the supporting analysis for both the Aeromaneuvering Orbit-to-Orbit Shuttle ...
Submitted in partial fulfillment of the requirements of the degree of Ocean Engineer at the Mass...
In this paper a study is made of vortex behaviour in axially asymmetrical hydraulic models. A brief ...
This thesis begins with a review of exo-electron emission i.e. the release of slow (<10eV) electrons...
In choosing the above title as the subject of a Thesis, I was impressed in my clinical work by the r...
The present research comprises: a. the development of an arithmetical trial and error method of find...
The downwash behind a wing may be computed from the system of vortices created by the wing and which...
The Thesis is divided primarily into three parts. In the first of these three parts is considered th...
Proper acoustic excitation of a single large-eddy break-up device can increase the resulting drag re...
Mainly as a result of the finding of the enquiry into the Whitehaven Colliery Explosion (1931), the ...
In part one the heredity of myopia,night-blindness and retinitis pigmentosa in association with othe...
Profile-drag coefficients published from tests in the N.A.C.A. variable-density tunnel (Technical Re...
The objective of this research is to increase the analytical capability of the existing TDK/BLM comp...
(a) That Pulmonary phthisis is an infectious disease and although hereditary predisposition has some...
This analysis computes for a predetermined airfoil and given Reynolds Number the course of the "disp...
Preliminary designs and the supporting analysis for both the Aeromaneuvering Orbit-to-Orbit Shuttle ...
Submitted in partial fulfillment of the requirements of the degree of Ocean Engineer at the Mass...
In this paper a study is made of vortex behaviour in axially asymmetrical hydraulic models. A brief ...
This thesis begins with a review of exo-electron emission i.e. the release of slow (<10eV) electrons...
In choosing the above title as the subject of a Thesis, I was impressed in my clinical work by the r...
The present research comprises: a. the development of an arithmetical trial and error method of find...
The downwash behind a wing may be computed from the system of vortices created by the wing and which...