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Wind-tunnel Investigation of External-flow Jet-augmented Double Slotted Flaps on a Rectangular Wing at an Angle of Attack of 0 Degree to High Momentum CoefficientsA wind-tunnel investigation has been made to determine the characteristics of external-flow jet-augmented double slotted flaps which appear suitable for application to airplanes with pod-mounted engines. The investigation included tests of the rectangular wing with an aspect ratio of 6 over a momentum-coefficient range from 0 to 28. Lift coefficients larger than the jet reaction in the lift direction were obtained with the external-flow jet-augmented double slotted flaps.
Document ID
19930085087
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Davenport, Edwin E
Date Acquired
August 16, 2013
Publication Date
September 1, 1957
Report/Patent Number
NACA-TN-4079
Report Number: NACA-TN-4079
Accession Number
93R14377
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
HIGH-LIFT DEVICES - COMPLETE WINGS
CONTROL, LONGITUDINAL
CONTROLS, FLAP-TYPE - COMPLETE WINGS

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