Transition flight experiments on a swept wing with suction
- 12 June 1989
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Numerical-perturbation technique for stability of flat-plate boundary layers with suctionAIAA Journal, 1986
- Stability of flow over axisymmetric bodies with porous suction stripsPhysics of Fluids, 1985
- Attachment-Line Flow on an Infinite Swept WingAIAA Journal, 1974
- Papers sought for SSA conventionxsThe Southern Speech Journal, 1967
- On the Flow Along Swept Leading EdgesAeronautical Quarterly, 1967