DEVELOPMENT efforts in both the B-70 and F-111 programmes have demonstrated that steady-state pressure distortion considerations are no longer sufficient to determine if the inlet/engine components of the propulsion system are compatible and operate in a stable manner for all flight conditions. Modern high speed aircraft operate in modes where the effects of shocks and boundary layers produce an inlet distortion environment which has considerable temporal variation. Early in a programme, the engine manufacturer must determine design requirements to enable operation with combined steady and unsteady flow distortions.
Inlet Flow Field Simulation Techniques for Engine/Compressor Testing
Aircraft Engineering and Aerospace Technology ; 42 , 11 ; 12-17
01.11.1970
6 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Inlet-engine compatibility testing techniques in ground test facilities
Tema Archiv | 1981
|Effect of steady state inlet temperature distortion on the engine compressor flow
Tema Archiv | 1986
|Flow measurement and simulation of a radial inlet for centrifugal compressor
Online Contents | 2015
|Inlet Flow Valve Engine Analyses
NTRS | 2004
|