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Autoren:
Selcan, Claudio 
Dokumenttyp:
Dissertation / Thesis 
Titel:
Advancement of the High-Enthalpy Free-Piston Reflected Shock Tunnel HELM for in situ Determination of Aerothermal Stagnation Conditions 
Betreuer:
Mundt, Christian, Univ.-Prof. Dr.-Ing. 
Gutachter:
Mundt, Christian, Univ.-Prof. Dr.-Ing.; Tanno, Hideyuki, Prof. 
Tag der mündlichen Prüfung:
25.05.2022 
Publikationsdatum:
09.08.2022 
Jahr:
2022 
Seiten (Monografie):
xxv, 233 
Sprache:
Englisch 
Schlagwörter:
Windkanal ; Stoßwellenrohr ; Windkanalströmung ; Kompression ; Enthalpie ; Hochtemperatur ; Messung ; Gitterspektroskopie ; Simulation 
Stichwörter:
High-enthalpy, High-temperature, High-pressure, Short-duration, Free-piston shock tunnel, LIGS, LITA, Laser-Diagnostics 
Abstract:
Experimental determination of test gas caloric quantities in high-enthalpy, hypersonic ground testing is impeded by excessive pressure and temperature levels as well as minimum test time scales of short-duration facilities. However, accurate knowledge of test gas conditions and stagnation enthalpy prior to nozzle expansion is vital to achieve a valid comparison of experimental data with numerical results. In order to facilitate a more accurate quantification of caloric nozzle inlet conditions in...    »
 
DDC-Notation:
629.13452 
Fakultät:
Fakultät für Luft- und Raumfahrttechnik 
Institut:
LRT 10 - Institut für Thermodynamik 
Professur:
Mundt, Christian 
Open Access ja oder nein?:
Ja / Yes