Accession Number : AD0097115

Title :   THE EFFECT OF BOUNDARY LAYER PROFILE, AIR SPEED, AND SYSTEM GEOMETRY ON THE STABILITY OF FLOW IN SUCTION SYSTEMS

Corporate Author : CORNELL AERONAUTICAL LAB INC BUFFALO NY

Personal Author(s) : TREANOR, C.E. ; FLAX, A.H.

Report Date : JUL 1956

Pagination or Media Count : 1

Descriptors :   *AERODYNAMIC CONFIGURATIONS, *BOUNDARY LAYER CONTROL, *DUCTS, DUCT INLETS, OPERATION.

Distribution Statement : APPROVED FOR PUBLIC RELEASE