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