Drag of shroud deployment bladder at Mach numbers of 8 to 20

Autor:	Henry Nagamatsu, Timothy Dominick, D. Messitt, Andrew Panetta, Marco Antonio Sala Minucci, Leik N. Myrabo
Rok vydání:	1999
Předmět:	Shock wave Physics Hypersonic speed Drag coefficient Expansion tunnel Pitot tube Mechanics law.invention symbols.namesake Mach number law Drag symbols Bow shock (aerodynamics) Marine engineering
Zdroj:	17th Applied Aerodynamics Conference.
DOI:	10.2514/6.1999-3206
Popis:	STRACT’ An investigation ‘of a Shroud Deployment System (SDS) bladder was conducted in the Rensselaer Polytechnic Institute 2+in .Hypersonic Shock Tunnel. The cut-rem investigation experimentally determined the axial drag coefficient for the bladder, while attached ~0 .$he SDS d-ge support, for nominal Mach numbers of 8 to 20 and stagnation temperatures up to 7400 “R Me&ements were made of the pitot pressure and the force applied to the bag by the j~ypynjc: ,flqw. i 10..
Databáze:	OpenAIRE
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