Conductive Electronic Weapons and Their Faults

Conductive Electronic Weapons and Their Faults
Author: Trevor Langevin
Publisher:
Total Pages: 242
Release: 2011-04
Genre: Science
ISBN: 9781257097340

Conductive Electronic Weapons and their faults is a book based on a Human Factors research project on the problems of using stun guns on commercial aircraft. The Robert Dziekanski incident happened at the Vancouver International Airport, and those findings were integrated into the research project. The author submitted all the results to the Braidwood Inquiry. The testimonies and other information revealed during the inquiry required multiple updates for unanswered questions and accusations to be addressed. The Braidwood Inquiry is not the only legal entity to find that the stun gun can cause death, it is the first where Taser International has not been able to change the final decision with legal action. The book centers around the authors submitted information to the inquiry, and has reached a new detailed hypothesis on how stun guns can cause death within seconds to days after a discharge. It also explains how the guns basic design can become faulty and output repeated arc phase levels of power.

Research and Engineering Problems

Research and Engineering Problems
Author: United States. Bureau of Naval Weapons
Publisher:
Total Pages: 128
Release: 1965
Genre: Marine engineering
ISBN:

This report is the third revision of the publication and supersedes NAVWEPS Report 7682A dated June, 1962.

An Integral Approach to Transient Heat-conduction Problems with Phase Transition

An Integral Approach to Transient Heat-conduction Problems with Phase Transition
Author: Tse-Fou Zien
Publisher:
Total Pages: 56
Release: 1975
Genre: Ablation (Aerothermodynamics)
ISBN:

An approximate method for studying transient heat-conduction problems is presented. Its application to various linear problems and nonlinear problems involving phase transitions is described by means of several idealized problems. The method is basically a refined version of the well-known Karman-Pohlhausen integral technique in boundary-layer theory, and represents a further development of the basic ideas previously exploited to calculate skin friction and heat transfer in boundary-layer flows. The approximate solutions obtained are extensively compared with existing exact solutions and those of the classical Karman-Pohlhausen method. From the simplicity and accuracy of the present method as demonstrated in the results, the potential utility of the method in providing simple, engineering solutions to complex aerodynamic heating problems can be inferred.