Accession Number : AD0616658

Title :   AN APPROXIMATE INVESTIGATION OF THE EFFECT OF BOUNDARY LAYER CONTROL PUMPING ON POWERPLANT PERFORMANCE,

Corporate Author : RAND CORP SANTA MONICA CALIF

Personal Author(s) : Kirkwood,T. F.

Report Date : 25 APR 1960

Pagination or Media Count : 7

Abstract : A first-order analysis is described of the effects of boundary layer bleed pumping on the performance of turbojet and turboprop powerplants.

Descriptors :   (*BOUNDARY LAYER CONTROL, PUMPS), (*AIRCRAFT ENGINES, BOUNDARY LAYER CONTROL), TURBOJET ENGINES, TURBOPROP ENGINES, BLEED SYSTEMS, DRAG, PERFORMANCE(ENGINEERING)

Distribution Statement : APPROVED FOR PUBLIC RELEASE