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Serial/Series Title:
NACA Wartime Reports
Collection:
National Advisory Committee for Aeronautics Collection
Wing-fuselage interference comparison of conventional and airfoil-type-fuselage combinations
Date: March 1, 1937
Creator: Sherman, Albert
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Permallink:digital.library.unt.edu/ark:/67531/metadc61155/
Tapered wings, tip stalling, and preliminary results from tests of the stall-control flap
Date: November 1, 1937
Creator: Jacobs, Eastman N
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Permallink:digital.library.unt.edu/ark:/67531/metadc61414/
Aerodynamic characteristics of a 4-engine monoplane showing effects of enclosing the engines in the wing and comparisons of tractor- and pusher-propeller arrangements
Date: April 1, 1938
Creator: Wilson, Herbert A , Jr
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Permallink:digital.library.unt.edu/ark:/67531/metadc62602/
Effects of simulated ice formation on the aerodynamic characteristics of an airfoil
Date: May 1, 1938
Creator: Gulick, Beverly G
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Permallink:digital.library.unt.edu/ark:/67531/metadc61800/
Comparison of free-spinning wind-tunnel results with corresponding full-scale spin results
Date: December 1, 1938
Creator: NEIHOUSE A I
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Permallink:digital.library.unt.edu/ark:/67531/metadc61109/
Preliminary report on the characteristics of the NACA 4400R series airfoils
Date: March 1, 1939
Creator: Sherman, Albert
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Permallink:digital.library.unt.edu/ark:/67531/metadc61446/
Acceleration, stress, and deflection measurements on the XB-15 bomber in gusty air
Date: June 1, 1939
Creator: Pearson, Henry A
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Permallink:digital.library.unt.edu/ark:/67531/metadc61098/
Preliminary Report on Laminar-Flow Airfoils and New Methods Adopted for Airfoil and Boundary-Layer Investigations
Date: June 1, 1939
Creator: Jacobs, Eastman N.
Description: Recent developments in airfoil-testing methods and fundamental air-flow investigations, as applied to airfoils, are discussed. Preliminary test results, obtained under conditions relatively free from stream turbulence and other disturbances, are presented. Suitable airfoils and airfoil-design principles were developed to take advantage of the unusually extensive laminar boundary layers that may be maintained under the improved testing conditions. The results are of interest mainly in range of below 6,000,000.
Contributing Partner: UNT Libraries Government Documents Department
Permallink:digital.library.unt.edu/ark:/67531/metadc61380/
Aerodynamic characteristics of a 4-engine monoplane showing comparison of air-cooled and liquid-cooled engine installations
Date: July 1, 1939
Creator: Wilson, Herbert A , Jr
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Permallink:digital.library.unt.edu/ark:/67531/metadc62601/
Heat-transfer tests of a steel cylinder barrel with aluminum fins
Date: August 1, 1939
Creator: Ellerbrock, Herman H , Jr
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Permallink:digital.library.unt.edu/ark:/67531/metadc61916/