Effect of idealized asymmetric inhibitor stubs on circumferential flow in the Space Shuttle SRM
- 1 January 1990
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Propulsion and Power
- Vol. 6 (1), 5-10
- https://doi.org/10.2514/3.23216
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Numerical Heat Transfer and Fluid FlowPublished by Informa UK Limited ,2018
- The numerical computation of turbulent flowsComputer Methods in Applied Mechanics and Engineering, 1974
- A calculation procedure for heat, mass and momentum transfer in three-dimensional parabolic flowsInternational Journal of Heat and Mass Transfer, 1972