Airfoil-Contour Modifications Based on (Epsilon)-Curve Method of Calculating Pressure Distribution Page: 1 of 25
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ARR No: T~0005
NATIONAL ADVISORY COMMITTEE
J i ASSIFfIAf!flH P.AhiLL[b,
ATRFOIL-CONTOUR MODIFICATIONS BASED ON c-CURVE
METHOD OF CALCULATING PRESSURE DISTRIBUTION
By Theodore Theodorsen
Langley Memorial Aeronautical Laboratory
Langley Field, Va.
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This document contains classified e .U] W ' be Imparted only to persons in toe military and naval
the National Defense of the Unit ,aflng Services of the United States, appropriate civiliar officers
of the Espionage Act, USC &lesion or and eployees of the Federal Government who have a legitimate
tne revelation of it t er to an unauthor- interest therein, and to United States citizens of known Iy-
ised person is prohibit information so classified alty and discretion who of necessity must be informed thereof.
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Theodorsen, Theodore. Airfoil-Contour Modifications Based on (Epsilon)-Curve Method of Calculating Pressure Distribution, report, July 1944; (digital.library.unt.edu/ark:/67531/metadc61280/m1/1/: accessed August 15, 2018), University of North Texas Libraries, Digital Library, digital.library.unt.edu; crediting UNT Libraries Government Documents Department.