Nozzle Plume/Shock Interaction Experimental and Computational Sonic Boom Analyses from the NASA Ames 9- by 7-Foot Supersonic Wind Tunnel

A wind tunnel test and a computational study were conducted to investigate the complex interactions between a supersonic nozzle plume and shock waves of differing strengths generated from various aft surfaces typical of supersonic aircraft. These analytically-defined aft surfaces were representative...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	Durston, Donald A., Cliff, Susan E., Denison, Marie F., Jensen, James C., Moran, Patrick J., Smith, Nathanial T., Heineck, James T., Schairer, Edward T., Kushner, Laura K., Castner, Raymond S., Elmiligui, Alaa, Carter, Melissa B., Winski, Courtney Spells, Shea, Patrick Ryan
Format:	Report
Sprache:	eng
Schlagworte:	Aerodynamics Fluid Mechanics And Thermodynamics
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!