Foreign Gas Injection into Three-Dimensional Stagnation Point Flows
Author:
Affiliation:
1. Northrop Corporation, Hawthorne, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.61706
Reference19 articles.
1. Diffusion-thermo effects in stagnation-point flow of air with injection of gases of various molecular weights into the boundary layer
2. Helium Injection Into the Boundary Layer at an Axisymmetric Stagnation Point
Cited by 5 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Three-dimensional turbulent boundary layer calculations - Exact and simplified solutions;8th Fluid and PlasmaDynamics Conference;1975-06-16
2. Heat and Mass Transfer at a General Three-Dimensional Stagnation Point;AIAA Journal;1975-06
3. Foreign Gas Injection at Windwardmost Meridians of Yawed Sharp Cones;AIAA Journal;1974-06
4. Mass transfer effects on the three-dimensional second-order boundary layer flow at the stagnation point of blunt bodies;Mechanics Research Communications;1974-01
5. Heat transfer—A review of 1972 literature;International Journal of Heat and Mass Transfer;1973-11
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