Accession Number:

AD0673985

Title:

INVESTIGATION OF VITIATED INLET-AIR EFFECTS ON TURBOJET ENGINE PERFORMANCE

Descriptive Note:

Technical rept.

Corporate Author:

NAVAL AIR PROPULSION TEST CENTER TRENTON NJ AERONAUTICAL TURBINE DEPT

Personal Author(s):

Report Date:

1968-07-01

Pagination or Media Count:

35.0

Abstract:

Laboratory test were conducted to investigate the effects of vitiated inlet-air on turbojet engine performance. The test vehicle was a J60-P-6 turbojet engine which was operated at sea level hot day inlet conditions for simulated flight Mach numbers of 0.0, 0.5, and 0.85. Effects of vitiated inlet- air were evaluated at vitiation levels of 1.7, 2.3, 3.0, and 3.5 percent.

Subject Categories:

  • Jet and Gas Turbine Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE