Zobrazeno 1 - 10
of 29
pro vyhledávání: '"Aaron Dufrene"'
Autor:
Scott A. Berry, Michael Semper, Andrew K. Riha, Charles D. Mullen, Helen L. Reed, Aaron Dufrene, Hermann F. Fasel
Publikováno v:
AIAA SCITECH 2022 Forum.
Publikováno v:
Journal of Thermophysics and Heat Transfer. 33:216-224
A database of heating and pressure measurements on a 7 deg half-angle cone in a high-enthalpy expansion tunnel in CO2 has been generated to support development and validation of computational model...
Publikováno v:
Journal of Spacecraft and Rockets. 55:382-402
The NASA Space Launch System vehicle is composed of four RS-25 liquid oxygen and hydrogen rocket engines in the core stage and two five-segment solid rocket boosters. Because of the complex nature ...
Publikováno v:
Journal of Thermophysics and Heat Transfer. 31:712-731
An extensive database of heating, pressure, and flowfield measurements on a 70 deg sphere-cone blunt-body geometry in high-enthalpy carbon-dioxide flow has been generated through testing in an expa...
Publikováno v:
22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference.
Publikováno v:
2018 AIAA Aerospace Sciences Meeting.
A database of heating and pressure measurements on a 7-deg half-angle cone in a highenthalpy expansion tunnel in CO2 has been generated to support development and validation of computational models to be employed in the design of future Mars missions
Publikováno v:
AIAA Journal. 53:573-587
The development of a nonintrusive microwave shock-speed measurement for expansion tunnels is presented, based on microwave standing-wave reflection. Testing is performed in a large-scale expansion-tunnel facility, with the goal of characterizing visc
Publikováno v:
47th AIAA Fluid Dynamics Conference.
Non-intrusive optical diagnostic imaging was used for the first time to visualize multi-rocket plume-induced reacting base flows to simulate launch vehicle ascent from sea-level to 250,000 ft. In particular, planar laser induced florescence (PLIF) an
Autor:
Matthew MacLean, Aaron Dufrene, Paul E. DesJardin, Eric C. Marineau, Ronald Parker, Michael Holden
Publikováno v:
Journal of Spacecraft and Rockets. 50:470-475
Publikováno v:
54th AIAA Aerospace Sciences Meeting.
The NASA Space Launch System (SLS) vehicle is composed of four RS-25 liquid oxygen-hydrogen rocket engines in the core-stage and two 5-segment solid rocket boosters and as a result six hot supersonic plumes interact within the aft section of the vehi