An effect of base hole size on dynamic test results
Abstract
This paper presents the dynamic test results of a flat-base sharp cone model hole diameters. The test Mach number is M = 5.047; cone semiangle is 10 deg; and the free-flow Reynolds number based on the model length is (2.2-13.3) x 10 to the 6th. The results show that the effect of the base hole diameter on test data really exists. In general, when the boundary-layer transition occurs on the aft surface of the model, the effect is obvious; with increasing hole diameter the static stability decreases and the dynamic stability increases. When the transition moves forward, the effect becomes unimportant. The mechanism of the effect is discussed briefly.
- Publication:
-
Acta Aerodynamica Sinica
- Pub Date:
- June 1986
- Bibcode:
- 1986AcAer...4..239L
- Keywords:
-
- Aerodynamic Interference;
- Conical Bodies;
- Dynamic Tests;
- Hole Geometry (Mechanics);
- Holes (Mechanics);
- Wind Tunnel Models;
- Wind Tunnel Tests;
- Boundary Layer Transition;
- Dynamic Stability;
- Static Stability;
- Supersonic Wind Tunnels;
- Fluid Mechanics and Heat Transfer