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Joined 2026-09-21
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Work by Robert M. Pinkerton
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Calculated and Measured Pressure Distributions over the Midspan Section of the NACA 4412 Airfoil by Robert M. Pinkerton
2026-11-05
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ntrs.nasa.gov/citations/19930091638
NACA-TR-563 (1937). NTRS
abstract
: 54
pressure
orifices
,
a
5
-by-30-
inch
model
, 17
angles
from −20 to 30 degrees,
Reynolds number
approximately
3
million; comparison with
potential-flow
calculations
.
0
The Characteristics of 78 Related Airfoil Sections from Tests in the Variable-Density Wind Tunnel by Eastman N. Jacobs and others
2026-11-05
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ntrs.nasa.gov/citations/19930091108
NACA Report 460, originally published November 1933; primary
PDF
:
ntrs.nasa.gov/api/citations/19930091108/downloads/19930091108.pdf
. Apparatus and Methods describes
duralumin
models
,
dimensions
,
Reynolds number
, tank
pressure
and measured
forces
/
moments
. The introduction and profile derivation explain systematic
variation
of
thickness
and
mean
-line form.
Total
articles
:
2