NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

Press Enter or click the Search button to begin your search.

Back to Results
Analysis of Factors Affecting Net Lift Increment Attainable with Trailing-Edge Split Flaps on Tailless Airplanes
Document ID
19930092727
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Maggin, Bernard
Date Acquired
September 6, 2013
Publication Date
September 1, 1944
Report/Patent Number
NACA-ARR-L4I18
NACA-WR-L-164
Report Number: NACA-ARR-L4I18
Report Number: NACA-WR-L-164
Accession Number
93R22017
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
WINGS, TAPERED
PITCHING MOMENTS
WINGS, HIGH-LIFT
AIRFOILS - AERODYNAMIC CENTER
WINGS - SWEEPBACK
LIFT COEFFICIENTS
WING FLAPS, SPLIT
AIRPLANES, TAILLESS
AIRFOILS - ASPECT RATIO

Related Records

There are no records associated with this record.
No Preview Available