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  Partner: UNT Libraries Government Documents Department
 Decade: 1930-1939
 Serial/Series Title: NACA Wartime Reports
 Collection: Technical Report Archive and Image Library
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
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
Tapered wings, tip stalling, and preliminary results from tests of the stall-control flap

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
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
Tests of Several Model Nacelle-Propeller Arrangements in Front of a Wing

Tests of Several Model Nacelle-Propeller Arrangements in Front of a Wing

Date: September 1, 1939
Creator: Mchugh, James G
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
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
Preliminary report on the characteristics of the NACA 4400R series airfoils

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
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