Unsteady Flows in Jet Engines: Proceedings of a Workshop Held at United Aircraft Research Laboratories, 11 and 12 July 1974F. O. Carta Project SQUID Headquarters, Jet Propulsion Center, School of Mechanical Engineering, Purdue University, 1974 - 511 páginas |
Contenido
W M Foley United Aircraft Research | 1 |
Thursday morning 11 July | 15 |
Unsteady Fluid Dynamic Response of an Isolated Rotor with | 75 |
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Términos y frases comunes
actuator disc aerodynamic airfoil amplitude analysis angle of attack annulus attenuation ATTN axial compressor axial velocity blade row boundary conditions boundary layer cascade chord circumferential distortion CIRCUMFERENTIAL POSITION constant diffuser disturbance dynamic effect engine equation exit experimental flow angle flow coefficient flow field flow rate function Horlock inlet angle inlet distortion leading edge lift lift coefficient linearized Mach number mean flow measured normal force operating oscillating P.O. Box parameter performance perturbation pitching moment plane predicted pressure distribution problem profiles quasi-steady radial ratio reduced frequency region Research rotating stall rotor rotor blades rotor inlet shown in Figure skin friction speed stage stagger angle stagnation pressure static pressure stator steady surge theory total pressure distortion trailing edge Turbomachines two-dimensional undistorted unsteady flow unsteady normal force values variation vortex vorticity wake Whitehead zero