Use of Slotted Walls to Reduce Subsonic Flow Wind-Tunnel Boundary Corrections in
- 1 December 1974
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 12 (12) , 1771-1772
- https://doi.org/10.2514/3.49608
Abstract
No abstract availableKeywords
This publication has 8 references indexed in Scilit:
- Some Measurements on Dynamic StallJournal of Aircraft, 1974
- Unsteady viscous flow on oscillating airfoilsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1974
- An Experimental Analysis of Dynamic Stall on an Oscillating AirfoilJournal of the American Helicopter Society, 1974
- Variational solution to the radiative equation by the use of a step function. II - Extension to nonlinear case by iteration method.AIAA Journal, 1973
- On the Mechanism of Dynamic StallJournal of the American Helicopter Society, 1972
- Wind-Tunnel Wall Interference Reduction by Streamwise Porosity DistributionAIAA Journal, 1972
- Variational solutions by the use of stepwise constant functions. I -Linear case.AIAA Journal, 1972
- Rectangular model for nongray radiative transferAIAA Journal, 1970