Zobrazeno 1 - 10
of 25
pro vyhledávání: '"Russ D. Rausch"'
Publikováno v:
AIAA Scitech 2019 Forum.
Publikováno v:
AIAA Scitech 2019 Forum.
Publikováno v:
AIAA Scitech 2019 Forum.
A wind tunnel test was conducted at the Ames Unitary Plan Wind Tunnel to characterize the transonic buffet environment of a generic launch vehicle forebody. The test examined a highly instrumented version of the Coe and Nute Model 11 test article fir
Publikováno v:
AIAA Scitech 2019 Forum.
Publikováno v:
54th AIAA Aerospace Sciences Meeting.
Time-varying buffet forcing functions arise from unsteady aerodynamic pressures and are one of many load environments, which contribute to the overall loading condition of a launch vehicle during ascent through the atmosphere. The buffet environment
Publikováno v:
54th AIAA Aerospace Sciences Meeting.
The 2014 test of the Space Launch System (SLS) Rigid Buffet Model conducted at the NASA Langley Transonic Dynamics Tunnel employed an extremely high number of unsteady pressure transducers. The high channel count provided an opportunity to examine th
Publikováno v:
Journal of Spacecraft and Rockets. 49:798-807
It is necessary to define the launch vehicle buffet loads to ensure that structural components and vehicle subsystems possess adequate strength, stress, and fatigue margins when the vehicle structural dynamic response to buffet forcing functions are
Publikováno v:
Journal of Spacecraft and Rockets. 49:822-833
The Ares I-X Flight Test Vehicle (FTV), launched in October 2009, carried with it over 243 buffet verification pressure sensors and was one of the most heavily instrumented launch vehicle flight tests. This flight test represented a unique opportunit
Publikováno v:
Journal of Spacecraft and Rockets. 49:788-797
A transonic wind tunnel test of the Ares I-X Rigid Buffet Model (RBM) identified a Mach number regime where unusually large buffet loads are present. A subsequent investigation identified the cause of these loads to be an alternating flow phenomenon
Autor:
Russ D. Rausch, Dimitri J. Mavriplis, William E. Milholen, Elizabeth M. Lee-Rausch, Neal T. Frink
Publikováno v:
Computers & Fluids. 38:511-532
A second international AIAA Drag Prediction Workshop (DPW-II) was organized and held in Orlando Florida on June 21-22, 2003. The primary purpose was to inves- tigate the code-to-code uncertainty. address the sensitivity of the drag prediction to grid