The performance of different boundary-layer bleed systems of a two-dimensional ramjet inlet has been investigated experimentally. The main objective of the study has been to identify the correlation between the inlet’s performance with different boundary-layer bleed geometries and the inlet’s internal flow. Experiments have therefore been carried out with varied boundary-layer bleed geometries at an angle of attack of 0 deg and at Mach numbers ranging from 2.5 to 3.5 in the Trisonic Wind Tunnel Cologne. The results are a continuation of an earlier study and show that the inlet’s performance and the effectiveness of boundary-layer bleed system depend on shock/boundary-layer interaction, unsteadiness of the flow, and flow separation.
Experimental Analyses of Inlet Characteristics of an Airbreathing Missile with Boundary-Layer Bleed
Journal of Propulsion and Power ; 31 , 1 ; 170-179
2015-01-01
Article (Journal)
Electronic Resource
English
Experimental Analyses of Inlet Characteristics of an Airbreathing Missile with Boundary-Layer Bleed
Online Contents | 2015
|Hypersonic Airbreathing Missile
NTRS | 1978
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