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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 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 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 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 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 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 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 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 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
Analysis of straight multicell wings on Cal-Tech analog computer

Analysis of straight multicell wings on Cal-Tech analog computer

Date: January 1, 1954
Creator: Benscoter, Stanley U & Macneal, Richard H
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Analysis of sweptback wings on Cal-Tech analog computer

Analysis of sweptback wings on Cal-Tech analog computer

Date: January 1954
Creator: Macneal, Richard H & Benscoter, Stanley U
Description: None
Contributing Partner: UNT Libraries Government Documents Department
An analysis of the stability and ultimate bending strength of multiweb beams with formed-channel webs

An analysis of the stability and ultimate bending strength of multiweb beams with formed-channel webs

Date: August 1954
Creator: Semonian, Joseph W & Anderson, Roger A
Description: None
Contributing Partner: UNT Libraries Government Documents Department
An analytical and experimental study of the transient response of a pressure-regulating relief valve in a hydraulic circuit

An analytical and experimental study of the transient response of a pressure-regulating relief valve in a hydraulic circuit

Date: March 1954
Creator: Gold, Harold & Otto, Edward W
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Analytical determination of the mechanism of an airplane spin recovery with different applied yawing moments by use of rotary-balance data

Analytical determination of the mechanism of an airplane spin recovery with different applied yawing moments by use of rotary-balance data

Date: December 1954
Creator: Burk, Sanger M , Jr
Description: None
Contributing Partner: UNT Libraries Government Documents Department
An analytical estimation of the effect of transpiration cooling on the heat-transfer and skin-friction characteristics of a compressible, turbulent boundary layer

An analytical estimation of the effect of transpiration cooling on the heat-transfer and skin-friction characteristics of a compressible, turbulent boundary layer

Date: December 1954
Creator: Rubesin, Morris W
Description: None
Contributing Partner: UNT Libraries Government Documents Department
An analytical investigation of airplane spin-recovery motion by use of rotary-balance aerodynamic data

An analytical investigation of airplane spin-recovery motion by use of rotary-balance aerodynamic data

Date: June 1954
Creator: Scher, Stanley H
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Application of two-dimensional vortex theory to the prediction of flow fields behind wings of wing body combinations at subsonic and supersonic speeds

Application of two-dimensional vortex theory to the prediction of flow fields behind wings of wing body combinations at subsonic and supersonic speeds

Date: September 1954
Creator: Rogers, Arthur WM
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Approximate effect of leading-edge thickness, incidence angle, and inlet mach number on inlet losses for high-solidity cascades of low cambered blades

Approximate effect of leading-edge thickness, incidence angle, and inlet mach number on inlet losses for high-solidity cascades of low cambered blades

Date: December 1954
Creator: Wright, Linwood C
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Bending tests on box beams having solid- and open-construction webs

Bending tests on box beams having solid- and open-construction webs

Date: August 1, 1954
Creator: Johnson, Aldie E , Jr
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Boundary-layer transition at Mach 3.12 with and without single roughness elements

Boundary-layer transition at Mach 3.12 with and without single roughness elements

Date: December 1, 1954
Creator: Brinich, Paul F
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Buckling of long square tubes in combined compression and torsion and comparison with flat-plate buckling theories

Buckling of long square tubes in combined compression and torsion and comparison with flat-plate buckling theories

Date: May 1, 1954
Creator: Peters, Roger W
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Burning times of magnesium ribbons in various atmospheres

Burning times of magnesium ribbons in various atmospheres

Date: December 1, 1954
Creator: Coffin, Kenneth P
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Calculated subsonic span loads and resulting stability derivatives of unswept and 45 degrees sweptback tail surfaces in sideslip and in steady roll

Calculated subsonic span loads and resulting stability derivatives of unswept and 45 degrees sweptback tail surfaces in sideslip and in steady roll

Date: October 1, 1954
Creator: Queijo, M J & Riley, Donald R
Description: None
Contributing Partner: UNT Libraries Government Documents Department
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