论文信息 - Nozzle Plume/Shock Interaction Sonic Boom Test Results from the NASA Ames 9- by 7-Foot Supersonic Wind Tunnel - 字舞流文

Nozzle Plume/Shock Interaction Sonic Boom Test Results from the NASA Ames 9- by 7-Foot Supersonic Wind Tunnel

Marie Denison | Melissa B. Carter | Raymond S. Castner | Derek J. Dalle | Susan E. Cliff | Patrick Shea | Alaa A. Elmiligui | Courtney S. Winski | Donald A. Durston | Patrick R. Shea | Brennan T. Blumenthal | Nathanial T. Smith | M. Denison | A. Elmiligui | N. Smith | S. Cliff | D. Durston | Brennan Blumenthal

[1] Shayan Moini-Yekta,et al. Wind Tunnel Model Design for Sonic Boom Studies of Nozzle Jet Flows with Shock Interactions , 2016 .

[2] James T. Heineck,et al. Stereo Photogrammetry Measurements of the Position and Attitude of a Nozzle-Plume/Shock-Wave Interaction Model in the NASA Ames 9- by 7-Ft Supersonic Wind Tunnel , 2017 .

[3] Marie Denison,et al. Computational Evaluations of Experimental Data for Sonic Boom Models with Nozzle Jet Flow Interactions , 2017 .