Aerodynamic characteristics of 15 NACA airfoil sections at seven Reynolds numbers from 0.7 x 106 to 9.0 x 106
By: Laurence K. Loftin and Hamilton A. Smith.
Contributors: Smith, Hamilton A.; United States. National Advisory Committee for Aeronautics.
Publisher: National Advisory Committee for Aeronautics
Published: 1949
Place of publication: Langley Air Force Base, Va
Number of pages: 75
Subjects: Aerodynamic characteristics; Airfoil profiles
Notes: Bibliographical references: p. 17.