Výsledky vyhledávání - "Alok K. Majumdar"

Axisymmetric Two-Dimensional Modeling of No Vent Filling of a Cryogenic Tank using Generalized Fluid System Simulation Program

Autor: Alok K. Majumdar, Andre LeClair, Jason W. Hartwig

Publikováno v: AIAA SCITECH 2023 Forum.

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::2d886e4404c23c850d885f1d1fa97787
https://doi.org/10.2514/6.2023-0848

Zobrazit plný text záznamu

Nodal Numerical Modeling of Submerged Helium Injection in a Cryogenic Propellant Tank

Autor: Michael Baldwin, Alok K. Majumdar, Andre LeClair

Publikováno v: AIAA SCITECH 2023 Forum.

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::2353e93b371d976253d1e526ffce5654
https://doi.org/10.2514/6.2023-0847

Zobrazit plný text záznamu

Modeling of Chill Down in Cryogenic Transfer Lines

Autor: Matthew F. Cross, Alok K. Majumdar, John C. Bennett, Ramesh B. Malla

Publikováno v: Journal of Spacecraft and Rockets. 39:284-289

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::eab9c81c33cb4753e5e2b5b6f6bf1e74
https://doi.org/10.2514/2.3810

Zobrazit plný text záznamu

Fast, Nonlinear Network Flow Solvers for Fluid and Thermal Transient Analysis

Autor: Dr. Alok K Majumdar, Prof. Sivaguru S Ravindran

Publikováno v: International Journal of Numerical Methods for Heat & Fluid Flow. 20

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::f483726ed51670b704068c43bd036ac7
https://doi.org/10.1108/96155391080001396

Zobrazit plný text záznamu

Semi-coupled flow and thermal analysis of the field joint during rapid pressurization of the redesigned solid rocket motor

Autor: Benny Ghaffarian, Robert Colbert, J. L. Clayton, Alok K. Majumdar

Publikováno v: 30th Aerospace Sciences Meeting and Exhibit.

A transient, semi-coupled, multi-dimensional thermal and flow analysis methodology was developed to predict the thermal/gas dynamic conditions in the field joint region of the Redesigned Solid Rocket Motor (RSRM). Transient temperature response, pres

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::74885083b5659b002c71356f6555e9b6
https://doi.org/10.2514/6.1992-856

Zobrazit plný text záznamu

Experimental determination of convective heat transfer coefficients in the separated flow region of the Space Shuttle Solid Rocket Motor

Autor: Alok K. Majumdar, R. Harold Whitesides, Susan L. Jenkins, David L. Bacchus

Publikováno v: 28th Aerospace Sciences Meeting.

A series of cold flow heat transfer tests was conducted with a 7.5-percent scale model of the Space Shuttle Rocket Motor (SRM) to measure the heat transfer coefficients in the separated flow region around the nose of the submerged nozzle. Modificatio

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::5a84892c443e46e874c0b5c2d84554f0
https://doi.org/10.2514/6.1990-43

Zobrazit plný text záznamu

Kniha

Tento výsledek nelze pro nepřihlášené uživatele zobrazit.
K zobrazení výsledku je třeba se přihlásit.

Vyhledávací nástroje:

Upřesnit hledání