NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Due to the lapse in federal government funding, NASA is not updating this website. We sincerely regret this inconvenience.

Back to Results
Charts for estimating downwash behind rectangular, trapezoidal, and triangular wings at supersonic speeds
Document ID
19930082761
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Haefeli, Rudolph C
Mirels, Harold
Cummings, John L
Date Acquired
August 16, 2013
Publication Date
August 1, 1950
Report/Patent Number
NACA-TN-2141
Report Number: NACA-TN-2141
Accession Number
93R12051
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
DOWNWASH
THEORIES - FLOW
WINGS, DELTA
WINGS, RECTANGULAR
LINEAR
LOAD DISTRIBTUION, WING-SPAN
WINGS, TRAPEZOIDAL
THEORIES - AIRFOILS
LIFTING-LINE
CHARTS - DOWNWASH
No Preview Available