Analytical Estimation of Infrared Signature of Converging and Converging-Diverging Nozzles of Jet Engine

2021 ◽  
Vol 14 (2) ◽  
Author(s):  
Nidhi Baranwal ◽  
Shripad P. Mahulikar
2000 ◽  
Author(s):  
Thomas Badinand ◽  
Heino Tamvel ◽  
Torsten H. Fransson

Abstract A method is developed to compute the infrared signature behind a jet engine. The radiative transfer equation is solved with the Finite Volume Method (FVM) based on a double discretization of the spatial and the directional domain. Then, by solving step-by-step for different wave numbers for all directions, the value of the intensity received by a point placed at infinity looking at the computational domain with a defined angle and at a defined wave number is obtained. The resulting values of the intensity for a jet engine plume case compared very well with results from a validated ray-tracing model. A sensibility analysis has been carried out to assess the influence of the spatial and directional mesh, as well as the composition of the gas mixture on the results. The method appeared to be a very powerful and practical tool to study the spectral radiative signature created by a flow with arbitrary geometry.


2017 ◽  
Vol 17 ◽  
pp. 245-252
Author(s):  
V. V. Somov

In carrying out an investigation into the explosion, among others, the investigative version of the use of a single-use reactive grenade launcher is being considered. The most common for criminal explosions are applied grenade launchers RPG-18, RPG-22, RPG-26. Their use is due to a number of such properties as small size and weight, which makes it possible to transfer them covertly, the range of the shot significantly exceeding the range of the hand grenade throw, the high detonating effect of the rocket grenade explosion. The single-use rocket launchers are generally of the same design. Their differences are in the features of the components construction and dimensional characteristics, which are given in the article. On the basis of expert practice, details ofgrenade launchers that remain at the site of the explosion and have the least damage are determined. These details are the objects of investigation of the explosion technical expertise. These objects include launchers of grenade launchers and rocket parts ofjet grenades. The design features of the launchers, their dimensional characteristics and marking symbols make it possible to determine their belonging to a specific type of jet grenade launchers. Missile parts of jet grenades differ in the form of the combustion chamber of the jet engine, nozzle, in the size ofthe outlet section of the nozzle, in the form and size of the stabilizerfeathers. To determine the belonging of the rocket part of the grenade to a specific type ofjet grenade launcher, it’s necessary to establish a set of structural features and dimensional characteristics. At considerable damage of the combustion chamber of the jet engine, as a rule, the nozzle block remains intact that allows to define diameter of critical section of a nozzle, and on it to establish type of the used single-use grenade launcher.


2000 ◽  
Author(s):  
A. Armendariz ◽  
D. Leith ◽  
M. Boundy ◽  
R. Goodman ◽  
L. Smith

2017 ◽  
Vol 25 (101) ◽  
pp. 74-75
Author(s):  
Alexey Viktorovich Kachura ◽  
◽  
Sergej V., Kolychev ◽  
Alexander Mikhailovich, Syanov
Keyword(s):  

Author(s):  
Robert Stowe ◽  
Sophie Ringuette ◽  
Pierre Fournier ◽  
Tracy Smithson ◽  
Rogerio Pimentel ◽  
...  

Author(s):  
Devdas Shetty ◽  
Tom Eppes ◽  
Nikolay Nazaryan ◽  
Claudio Campana ◽  
Jun Kondo

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