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 Decade: 1920-1929
 Serial/Series Title: NACA Technical Notes
 Collection: Technical Report Archive and Image Library
Tests on duralumin columns for aircraft construction

Tests on duralumin columns for aircraft construction

Date: November 1, 1924
Creator: Lee, John G
Description: The following paper is based on the results of tests, upon duralumin columns, contained in two theses presented to the Department of Civil and Sanitary Engineering of the Massachusetts Institute of Technology.
Contributing Partner: UNT Libraries Government Documents Department
On the Resistance of spheres and ellipsoids in wind tunnels

On the Resistance of spheres and ellipsoids in wind tunnels

Date: January 1, 1921
Creator: Riabouchinsky, D P
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Measurement of the moments of inertia of full scale airplanes

Measurement of the moments of inertia of full scale airplanes

Date: January 1, 1927
Creator: Green, M W
Description: None
Contributing Partner: UNT Libraries Government Documents Department
The influence of inlet air temperature and jacket water temperature on initiating combustion in a high speed compression ignition engine

The influence of inlet air temperature and jacket water temperature on initiating combustion in a high speed compression ignition engine

Date: March 1, 1924
Creator: Matthews, Robertson
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Tests of the N.P.L. airship models in the variable density wind tunnel

Tests of the N.P.L. airship models in the variable density wind tunnel

Date: September 1, 1927
Creator: Higgins, George J
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Development of the inflow theory of the propeller

Development of the inflow theory of the propeller

Date: November 1, 1920
Creator: Betz, A
Description: None
Contributing Partner: UNT Libraries Government Documents Department
The Characteristics of the N.A.C.A 97, Clark Y, and N.A.C.A. M6 Airfoils with Particular Reference to the Angle of Attack

The Characteristics of the N.A.C.A 97, Clark Y, and N.A.C.A. M6 Airfoils with Particular Reference to the Angle of Attack

Date: December 1, 1927
Creator: Higgins, George J.
Description: No abstract available.
Contributing Partner: UNT Libraries Government Documents Department
Effect of protruding gasoline tanks upon the characteristics of an airfoil

Effect of protruding gasoline tanks upon the characteristics of an airfoil

Date: October 1, 1926
Creator: Jacobs, Eastman N
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Precision of wing sections and consequent aerodynamic effects

Precision of wing sections and consequent aerodynamic effects

Date: January 1, 1927
Creator: Rizzo, Frank
Description: None
Contributing Partner: UNT Libraries Government Documents Department
The effect of tube length upon the recorded pressures from a pair of static orifices in a wing panel

The effect of tube length upon the recorded pressures from a pair of static orifices in a wing panel

Date: November 1, 1926
Creator: Carroll, T
Description: None
Contributing Partner: UNT Libraries Government Documents Department
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