Accession Number:

ADP011111

Title:

Thrust Vectoring for Advanced Fighter Aircraft - High Angle of Attack Intake Investigations -

Descriptive Note:

Corporate Author:

DAIMLER CHRYSLER AEROSPACE AG MUNICH (GERMANY)

Personal Author(s):

Report Date:

2001-06-01

Pagination or Media Count:

14.0

Abstract:

In this paper the results of investigations will be presented which dealt with the determination of intake flows at high and very high angles of attack. The overall approach comprised of experimental and numericalCFD investigations will be detailed. Results and comparisons between flows at small and large angles of attack will be used to try to clarify the origin of possible disturbances in the intake flow. Intake bleed and the flow losses at the intake entrance are identified as major components contributing to the quality of the intake flow at the engine face.

Subject Categories:

  • Flight Control and Instrumentation
  • Rocket Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE