Removal of the reflected pressure pulses from the end of a shock tube (U) / by W.A. Jones and F.L. McCallum. : DR52-1/1-1970E-PDF
Summarizes the data obtained during the development of a reflection eliminator to prevent positive or negative pressure pulses, generated by shock wave interaction with the end of a shock tube, propagating back up the expansion chamber. The study was shown that both the reflected positive and negative pressure pulses can be reduced to a very small amplitude by a flat plate placed at a predetermined distance downstream of the open end of the expansion chamber, or by a screen with adjustable openings attached to the open end of the expansion chamber.
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Ministère/Organisme | Defence Research Establishment Suffield, issuing body. |
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Titre | Removal of the reflected pressure pulses from the end of a shock tube (U) / by W.A. Jones and F.L. McCallum. |
Titre de la série | Suffield technical note ; no. 257 |
Type de publication | Série - Voir l'enregistrement principal |
Langue | [Anglais] |
Format | Électronique |
Document électronique | |
Note(s) | "Project no. D-16-01-27, D-95-11-68". Digitized edition from print [produced by Defence Research and Development Canada]. |
Information sur la publication | Ralston, Alberta : Defence Research Establishment Suffield, April 1970. |
Auteur / Contributeur | Jones, W. A., author. |
Description | 1 online resource (10, [15] pages) : illustrations, charts |
Numéro de catalogue |
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Numéro de catalogue du ministère | DRES-TN-257 |
Descripteurs | Shock tubes. Shock waves. Explosives, Military -- Testing. Military research -- Canada. Tubes à choc. Ondes de choc. Explosifs militaires -- Tests. Recherche militaire -- Canada. |
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