@inproceedings{Mon\~{a}2011Hypervelocityb,
title = {Design of a Non-Diaphragm Driver for the UFABC Hypersonic Wind Tunnel},
author = {Mon\~{a} Hegel Benetti and Israel Silveira R\^{e}go},
url = {https://www.sige.ita.br/edicoes-anteriores/2011/st/IV_1.pdf},
year = {2011},
date = {2011-01-01},
booktitle = {Simp\'{o}sio de Aplica\c{c}\~{o}es Operacionais em \'{A}reas de Defesa 2011 (SIGE2011)},
abstract = {Laboratory study of hypersonic vehicles and air- breathing engines such as “waveriders” and scramjets demands experimental facilities capable of simulating fligths at Mach numbers in excess of 5 with high stagnation temperatures. This paper shows the design and operational principle of a non- diaphragm driver for a hypersonic impulse wind tunnel at Universidade Federal do ABC (UFABC). Such a diaphragmless driver operates without the necessity of using the conventional the non- diaphragm. Experimental advantages of using diaphragm driver are much cleaner flowfields, no erratic runs, good reproducibility and costliness setup of the facility within minutes. Keywords Hypervelocity, Wind tunnel, Design.},
keywords = {design, Hypervelocity, Wind tunnel},
pubstate = {published},
tppubtype = {inproceedings}
}
Laboratory study of hypersonic vehicles and air- breathing engines such as “waveriders” and scramjets demands experimental facilities capable of simulating fligths at Mach numbers in excess of 5 with high stagnation temperatures. This paper shows the design and operational principle of a non- diaphragm driver for a hypersonic impulse wind tunnel at Universidade Federal do ABC (UFABC). Such a diaphragmless driver operates without the necessity of using the conventional the non- diaphragm. Experimental advantages of using diaphragm driver are much cleaner flowfields, no erratic runs, good reproducibility and costliness setup of the facility within minutes. Keywords Hypervelocity, Wind tunnel, Design.
