Design of a Supersonic Wind Tunnel

This study was a preliminary work of how to implement a rocket with sensors in order to get information about the flight.

Bibliographic Details
Authors:	Torunogullari, Altay, Schneider, Maxime, Pal, Itsvan, Tristancho Martínez, Joshua\|\|\|0000-0003-2440-255X
Format:	report
Publication Date:	2011
Country:	España
Institution:	Universitat Politècnica de Catalunya (UPC)
Repository:	UPCommons. Portal del coneixement obert de la UPC
Language:	English
OAI Identifier:	oai:upcommons.upc.edu:2117/16017
Online Access:	https://hdl.handle.net/2117/16017
Access Level:	Open access
Keyword:	Wind tunnel models High-speed aeronautics Túnels aerodinàmics Àrees temàtiques de la UPC::Aeronàutica i espai::Aerodinàmica::Tunels aerodinàmics

Description
Summary:	This study was a preliminary work of how to implement a rocket with sensors in order to get information about the flight.