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  Partner: UNT Libraries Government Documents Department
 Serial/Series Title: NACA Wartime Reports
 Collection: Technical Report Archive and Image Library
Wing-fuselage interference comparison of conventional and airfoil-type-fuselage combinations

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
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
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
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
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
Pressure drop in tank and float vent tubes on diving airplanes

Pressure drop in tank and float vent tubes on diving airplanes

Date: January 1, 1939
Creator: Waldron, C D
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
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 1939
Creator: Pearson, Henry A
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
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
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
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
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
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
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
Boundary-Layer Transition on the N.A.C.A. 0012 and 23012 Airfoils in the 8-Foot High-Speed Wind Tunnel

Boundary-Layer Transition on the N.A.C.A. 0012 and 23012 Airfoils in the 8-Foot High-Speed Wind Tunnel

Date: January 1, 1940
Creator: Becker, John V
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Estimation of critical speeds of airfoils and streamline bodies

Estimation of critical speeds of airfoils and streamline bodies

Date: March 1, 1940
Creator: Wright, Ray H
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Consideration of auxiliary jet propulsion for assisting take-off

Consideration of auxiliary jet propulsion for assisting take-off

Date: May 1, 1940
Creator: Turner, L Richard
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Experimental investigation to determine the relative magnitude of vertical and horizontal gusts in the atmosphere

Experimental investigation to determine the relative magnitude of vertical and horizontal gusts in the atmosphere

Date: July 1, 1940
Creator: Donely, Philip
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Heat transfer tests of a steel cylinder barrel with aluminum fins with improved bonding between steel barrel and aluminum base

Heat transfer tests of a steel cylinder barrel with aluminum fins with improved bonding between steel barrel and aluminum base

Date: July 1, 1940
Creator: Ellerbrock, Herman H , Jr
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Requirements for unit fuel-injection systems

Requirements for unit fuel-injection systems

Date: July 1, 1940
Creator: Marsh, Edred T
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Heat-transfer tests of two steel cylinder barrels with aluminum fins manufactured by factory production method

Heat-transfer tests of two steel cylinder barrels with aluminum fins manufactured by factory production method

Date: August 1, 1940
Creator: Ellerbrock, Herman H , Jr
Description: None
Contributing Partner: UNT Libraries Government Documents Department
High-speed drag tests of several fuselage shapes in combination with a wing

High-speed drag tests of several fuselage shapes in combination with a wing

Date: August 1, 1940
Creator: Draley, Eugene C
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Investigation of the boundary layer about a symmetrical airfoil in a wind tunnel of low turbulence

Investigation of the boundary layer about a symmetrical airfoil in a wind tunnel of low turbulence

Date: August 1, 1940
Creator: Von Doenhoff, Albert E
Description: None
Contributing Partner: UNT Libraries Government Documents Department
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