Nonuniform velocity profiles imposed on the propulsion system fan can cause fan blade stresses and thrust losses. This paper presents a theoretical parametric study of the effects of inlets with 0 deg and 90 deg nozzle deflection on the velocity profile at a hypothetical fan. The parameters investigated are fan-to-nozzle spacing and inlet centerline offset. The interaction between the inlet and nozzle is also investigated. The study is made using a two-dimensional analysis
Theoretical fan velocity distortions due to inlets and nozzles
Workshop on V/STOL Aerodynamics ; 1979 ; Monterey, CA
01.05.1979
Aufsatz (Konferenz)
Keine Angabe
Englisch
Inlets and Nozzles for Aerospace Engines
NTIS | 1971
Aerodynamic performance of flared fan nozzles used as inlets
TIBKAT | 1976
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