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  Partner: UNT Libraries Government Documents Department
 Decade: 1930-1939
 Serial/Series Title: NACA Wartime Reports
 Collection: National Advisory Committee for Aeronautics Collection
Acceleration, stress, and deflection measurements on the XB-15 bomber in gusty air

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
Aerodynamic characteristics of a 4-engine monoplane showing comparison of air-cooled and liquid-cooled engine installations

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 & Silverstein, Abe
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Aerodynamic characteristics of a 4-engine monoplane showing effects of enclosing the engines in the wing and comparisons of tractor- and pusher-propeller arrangements

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
Comparison of free-spinning wind-tunnel results with corresponding full-scale spin results

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
The Effect of Streamlining the Aterbody of an NACA Cowling

The Effect of Streamlining the Aterbody of an NACA Cowling

Date: December 1, 1939
Creator: Naiman, Irven
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Effects of propellers and of vibration on the extent of laminar flow on the NACA 27-212 airfoil

Effects of propellers and of vibration on the extent of laminar flow on the NACA 27-212 airfoil

Date: October 1, 1939
Creator: Gaydos, M Edward
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Effects of simulated ice formation on the aerodynamic characteristics of an airfoil

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
Ground-cooling and flight tests of an airplane equipped with a nose-blower engine cowling

Ground-cooling and flight tests of an airplane equipped with a nose-blower engine cowling

Date: October 1, 1939
Creator: Turner, L I , Jr
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Heat-transfer tests of a steel cylinder barrel with aluminum fins

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
Preliminary Report on Laminar-Flow Airfoils and New Methods Adopted for Airfoil and Boundary-Layer Investigations

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
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