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  Partner: UNT Libraries Government Documents Department
 Decade: 1950-1959
 Year: 1954
 Serial/Series Title: NACA Technical Notes
 Collection: National Advisory Committee for Aeronautics Collection
Additional static and fatigue tests of high-strength aluminum-alloy bolted joints

Additional static and fatigue tests of high-strength aluminum-alloy bolted joints

Date: July 1, 1954
Creator: Hartmann, E C; Holt, Marshall & Eaton, I D
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Aerodynamic characteristics of the NACA 64-010 and 0010-1.10 40/1.051 airfoil sections at Mach numbers from 0.30 to 0.85 and Reynolds numbers from 4.0 x 10(exp. 6) to 8.0 x 10(exp. 6)

Aerodynamic characteristics of the NACA 64-010 and 0010-1.10 40/1.051 airfoil sections at Mach numbers from 0.30 to 0.85 and Reynolds numbers from 4.0 x 10(exp. 6) to 8.0 x 10(exp. 6)

Date: August 1, 1954
Creator: Loftin, Laurence K , Jr
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Aerodynamic forces, moments, and stability derivatives for slender bodies of general cross section

Aerodynamic forces, moments, and stability derivatives for slender bodies of general cross section

Date: November 1, 1954
Creator: Sacks, Alvin H
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Aerodynamic forces, moments, and stability derivatives for slender bodies of general cross section

Aerodynamic forces, moments, and stability derivatives for slender bodies of general cross section

Date: November 1, 1954
Creator: Sacks, Alvin H.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Aerodynamic investigation of a four-blade propeller operating through an angle-of-attack range from 0 to 180 degrees

Aerodynamic investigation of a four-blade propeller operating through an angle-of-attack range from 0 to 180 degrees

Date: June 1, 1954
Creator: Mclemore, H Clyde & Cannon, Michael D
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Aerodynamic loads on a leading-edge flap and a leading-edge slat on the NACA 64A010 airfoil section

Aerodynamic loads on a leading-edge flap and a leading-edge slat on the NACA 64A010 airfoil section

Date: June 1, 1954
Creator: Kelly, John A & Mccullough, George B
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Aerodynamics of slender wings and wing-body combinations having swept trailing edges

Aerodynamics of slender wings and wing-body combinations having swept trailing edges

Date: March 1, 1954
Creator: Mirels, Harold
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Airfoil section characteristics at high angles of attack

Airfoil section characteristics at high angles of attack

Date: August 1, 1954
Creator: Loftin, Laurence K , Jr
Description: None
Contributing Partner: UNT Libraries Government Documents Department
The Ames 10- by 14-inch supersonic wind tunnel

The Ames 10- by 14-inch supersonic wind tunnel

Date: January 1, 1954
Creator: Eggers, A J & Nothwang, George J
Description: None
Contributing Partner: UNT Libraries Government Documents Department
An analysis of shock-wave cancellation and reflection for porous walls which obey an exponential mass-flow pressure-difference relation

An analysis of shock-wave cancellation and reflection for porous walls which obey an exponential mass-flow pressure-difference relation

Date: August 1, 1954
Creator: Spiegel, Joseph M & Tunnell, Phillips J
Description: None
Contributing Partner: UNT Libraries Government Documents Department
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