Affiliation:
1. NASA Langley Research Center
Publisher
American Institute of Aeronautics and Astronautics
Reference18 articles.
1. On the Flow Along Swept Leading Edges
2. Some observations of the transition process on the windward face of a long yawed cylinder
3. Anderson, B. T., and Meyer Jr, R. R. “Effects of Wing Sweep on In-flight Boundary-layer Transition for a Laminar Flow Wing at Mach Numbers from 0.60 to 0.79,” NASA STI/Recon Technical Report N, Vol.91, 1990, p. 24555.
4. Computational Design and Analysis of a Transonic Natural Laminar Flow Wing for a Wind Tunnel Model