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Pressure Distribution of a Large Semispan Tilting Wing with 0.4-diameter-chord, Single- Slotted Flap, and a Single Propeller 0.22 Chord Below WingAerodynamic pressure distribution on semispan tilting wing-propeller combination of V/STOL aircraft
Document ID
19690031487
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Fink, M. P. (NASA Langley Research Center Hampton, VA, United States)
Smith, C. C., Jr. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1969
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-5481
Report Number: NASA-TN-D-5481
Accession Number
69N40876
Funding Number(s)
CONTRACT_GRANT: 721-01-11-04-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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