Experimental study of the separating confluent boundary-layer. Volume 2: Experimental data. Appendices A-E: Data supplement
Abstract
A supplement to NASA document N84-20481 is presented in the form of appendices A, B, C, D, and E, which contain the LV-derived boundary-layer and wake data for approximately 30,000 combinations of airfoil geometric locations and configurations in the form of velocity vectors, turbulence intensities, and Reynolds shear stresses. The appendices are provided on a floppy disk. The original document discussed an experimental low speed study of the separating confluent boundary layer on a NASA GAW-1 high lift airfoil.
- Publication:
-
NASA STI/Recon Technical Report N
- Pub Date:
- March 1983
- Bibcode:
- 1983STIN...9324531B
- Keywords:
-
- Boundary Layer Separation;
- Convergence;
- Flow Visualization;
- Gaw-1 Airfoil;
- Turbulent Boundary Layer;
- Velocity Measurement;
- Laser Doppler Velocimeters;
- Leading Edge Slats;
- Shear Stress;
- Trailing Edge Flaps;
- Turbulence;
- Wakes;
- Fluid Mechanics and Heat Transfer