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Wind-tunnel investigation of boundary-layer control by suction on NACA 655-424 airfoil with double slotted flap
Document ID
19930082300
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Racisz, Stanley F
Quinn, John H
Date Acquired
August 16, 2013
Publication Date
June 1, 1948
Report/Patent Number
NACA-TN-1631
Report Number: NACA-TN-1631
Accession Number
93R11590
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
WIND TUNNEL TESTS - NACA - PRESSURE, LOW-TURBULENCE WORK CARRIED ON ATLMAL
AIRFOILS - CHARACTERISTICS EFFECT OF SURFACE ROUGHNESS
PRESSURE DISTRIBUTION - AIRFOILS - NACA 655-424
WIND TUNNEL TESTS - NACA - LOW-TURBULENCE (7 1/2'X 3') WORK CARRIED ON AT LMAL
BOUNDARY LAYER CONTROL - AIRFOILS - NACA 655-424
AIRFOILS - NACA 655-424-CHAR & ORDINATES LOW-DRAG WING FLAPS
BOUNDARY LAYER CONTROL - SUCTION-SLOTS

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