## Basic studies of rotating stall and an investigation of flow-instability sensing devices, Part 1Air Force Aero-propulsion Laboratory, Research and Technology Division, Air Force Systems Command, 1965 - Science |

### What people are saying - Write a review

We haven't found any reviews in the usual places.

### Common terms and phrases

120 degrees actuator characteristics adverse pressure gradient agreement airfoil amplitude analytical approximate axial flow compressors blade rows Boundary-Layer Velocity Profiles calculations configuration CORNELL AERONAUTICAL LABORATORY criterion data of Reference determinant downstream-moving wall Equation II-26 Equation III-39 experimental data fluid High Solidity hot wire inception of rotating investigation isolated rotor iteration laminar separation leading edge leading-edge stall linear Magnus effect minimum pressure moving wall neutral stability NONDIMENSIONAL ROTOR ROTATION obtained parameters position of minimum position of separation predictions pressure distribution Profiles on Shrouded Reference 11 rotating stall ROTOR ROTATION VELOCITY second root Security Classification separation point shown in Figure Shrouded Rotating Cylinder skin friction small disturbance solution SPONSORING MILITARY stability equation stability theory stagnation point static pressure difference stationary wall stator stream function surface tangential component theory and experiment two-actuator unstable roots unsteady flow upstream-moving wall velocity component vorticity wall moving downstream wall velocity wave number