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Aerodynamic characteristics of twin-propeller deflected-slipstream STOL airplane model with boundary-layer control on inverted v-tail / by Richard J. Margason and Garl L. Gentry, Jr.
Author:
Margason, Richard J.
Published:
Washington, D.C. : National Aeronautics and Space Administration, November 1968.
Physical Description:
1 online resource (179 pages) : illustrations
Additional Creators:
Gentry, Garl L.
,
United States. National Aeronautics and Space Administration
, and
Langley Research Center
Access Online
purl.fdlp.gov
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Series:
NASA technical note ; NASA TN D-4856
Restrictions on Access:
Free-to-read Unrestricted online access
Report Numbers:
NAS 1.14:D-4856
Subject(s):
Short take-off and landing aircraft
Boundary layer control
Propellers, Aerial
Airplanes
—
Tail surfaces
Aerodynamics
Note:
"November1968."
Bibliography Note:
Includes bibliographical references (page 16).
View MARC record
| catkey: 32505336