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  Partner: UNT Libraries Government Documents Department
 Decade: 1950-1959
 Year: 1955
 Serial/Series Title: NACA Technical Notes
 Collection: National Advisory Committee for Aeronautics Collection
An accurate and rapid method for the design of supersonic nozzles

An accurate and rapid method for the design of supersonic nozzles

Date: February 1955
Creator: Beckwith, Ivan E & Moore, John A
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Acoustic analysis of ram-jet buzz

Acoustic analysis of ram-jet buzz

Date: November 1955
Creator: Mirels, Harold
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Acoustic radiation from two-dimensional rectangular cutouts in aerodynamic surfaces

Acoustic radiation from two-dimensional rectangular cutouts in aerodynamic surfaces

Date: August 1955
Creator: Krishnamurty, K
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Acoustical treatment for the NACA 8- by 6-foot supersonic propulsion wind tunnel

Acoustical treatment for the NACA 8- by 6-foot supersonic propulsion wind tunnel

Date: June 1955
Creator: Beranek, Leo L; Labate, Samuel & Ingard, Uno
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Aerodynamic characteristics of a small-scale shrouded propeller at angles of attack from 0 to 90 degrees

Aerodynamic characteristics of a small-scale shrouded propeller at angles of attack from 0 to 90 degrees

Date: November 1955
Creator: Parlett, Lysle P
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Aerodynamic characteristics of NACA 0012 airfoil section at angles of attack from 0 degrees to 180 degrees

Aerodynamic characteristics of NACA 0012 airfoil section at angles of attack from 0 degrees to 180 degrees

Date: January 1955
Creator: Critzos, Chris C; Heyson, Harry H & Boswinkle, Robert W , Jr
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Aerodynamic characteristics of several 6-percent-thick airfoils at angles of attack from 0 degrees to 20 degrees at high subsonic speeds

Aerodynamic characteristics of several 6-percent-thick airfoils at angles of attack from 0 degrees to 20 degrees at high subsonic speeds

Date: May 1955
Creator: Daley, Bernard N & Lord, Douglas R
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Aerodynamics of a rectangular wing of infinite aspect ratio at high angles of attack and supersonic speeds

Aerodynamics of a rectangular wing of infinite aspect ratio at high angles of attack and supersonic speeds

Date: July 1955
Creator: Martin, John C & Malvestuto, Frank S , Jr
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Amplitude of supersonic diffuser flow pulsations

Amplitude of supersonic diffuser flow pulsations

Date: October 1, 1955
Creator: Sterbentz, William H & Davids, Joseph
Description: None
Contributing Partner: UNT Libraries Government Documents Department
An analysis of acceleration, airspeed, and gust-velocity data from a four-engine transport airplane in operations on an eastern United States route

An analysis of acceleration, airspeed, and gust-velocity data from a four-engine transport airplane in operations on an eastern United States route

Date: September 1, 1955
Creator: Coleman, Thomas L & Fetner, Mary W
Description: None
Contributing Partner: UNT Libraries Government Documents Department
An analysis of acceleration, airspeed, and gust-velocity data from one type of four-engine transport airplane operated over two domestic routes

An analysis of acceleration, airspeed, and gust-velocity data from one type of four-engine transport airplane operated over two domestic routes

Date: October 1, 1955
Creator: Coleman, Thomas L & Copp, Martin R
Description: None
Contributing Partner: UNT Libraries Government Documents Department
An analysis of accelerations, airspeeds, and gust velocities from three commercial operations of one type of medium-altitude transport airplane

An analysis of accelerations, airspeeds, and gust velocities from three commercial operations of one type of medium-altitude transport airplane

Date: March 1, 1955
Creator: Coleman, Thomas L; Copp, Martin R; Engel, Jerome N & Walker, Walter G
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Analysis of accelerations, gust velocities, and airspeeds from operations of a twin-engine transport airplane on a transcontinental route from 1950 to 1952

Analysis of accelerations, gust velocities, and airspeeds from operations of a twin-engine transport airplane on a transcontinental route from 1950 to 1952

Date: February 1, 1955
Creator: Coleman, Thomas L & Walker, Walter G
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Analysis of behavior of simply supported flat plates compressed beyond the buckling load into the plastic range

Analysis of behavior of simply supported flat plates compressed beyond the buckling load into the plastic range

Date: February 1955
Creator: Mayers, J & Budiansky, Bernard
Description: An analysis is presented of the postbuckling behavior of a simply supported square flat plate with straight edges compressed beyond the buckling load into the plastic range. The method of analysis involves the application of a variational principle of the deformation theory of plasticity in conjunction with computations carried out on a high-speed calculating machine. Numerical results are obtained for several plate proportions and for one material. The results indicate plate strengths greater than those that have been found experimentally on plates that do not satisfy straight-edge conditions. (author).
Contributing Partner: UNT Libraries Government Documents Department
Analysis of ear formation in deep-drawn cups

Analysis of ear formation in deep-drawn cups

Date: May 1955
Creator: Mcevily, Arthur J , Jr
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Analysis of errors introduced by several methods of weighting nonuniform duct flows

Analysis of errors introduced by several methods of weighting nonuniform duct flows

Date: March 1955
Creator: Wyatt, Demarquis D
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Analysis of fully developed turbulent heat transfer and flow in an annulus with various eccentricities

Analysis of fully developed turbulent heat transfer and flow in an annulus with various eccentricities

Date: May 1955
Creator: Deissler, Robert G & Taylor, Maynard F
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Analysis of laminar forced-convection heat transfer in entrance region of flat rectangular ducts

Analysis of laminar forced-convection heat transfer in entrance region of flat rectangular ducts

Date: January 1955
Creator: Sparrow, E M
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Analysis of stresses in the plastic range around a circular hole in a plate subjected to uniaxial tension

Analysis of stresses in the plastic range around a circular hole in a plate subjected to uniaxial tension

Date: October 1955
Creator: Budiansky, Bernard & Vidensek, Robert J
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Analysis of the horizontal-tail loads measured in flight on a multiengine jet bomber

Analysis of the horizontal-tail loads measured in flight on a multiengine jet bomber

Date: September 1955
Creator: Aiken, William S & Wiener, Bernard
Description: None
Contributing Partner: UNT Libraries Government Documents Department
An Analysis of the Stability and Ultimate Compressive Strength of Short Sheet-Stringer Panels with Special Reference to the Influence of Riveted Connection Between Sheet and Stringer

An Analysis of the Stability and Ultimate Compressive Strength of Short Sheet-Stringer Panels with Special Reference to the Influence of Riveted Connection Between Sheet and Stringer

Date: March 1955
Creator: Semonian, Joseph W & Peterson, James P
Description: A method of strength analysis of short sheet-stringer panels subjected to compression is presented which takes into account the effect that the riveted attachments between the plate and the stiffeners have on the strength of the panels. An analysis of experimental data shows that panel strength is highly influenced by rivet pitch, diameter, and location and that the degree of influence for a given riveting depends on the panel configuration and panel material. (author).
Contributing Partner: UNT Libraries Government Documents Department
Analysis of two-dimensional compressible-flow loss characteristics downstream of turbomachine blade rows in terms of basic boundary-layer characteristics

Analysis of two-dimensional compressible-flow loss characteristics downstream of turbomachine blade rows in terms of basic boundary-layer characteristics

Date: July 1955
Creator: Stewart, Warner L
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Analytic determination of the discharge coefficients of flow nozzles

Analytic determination of the discharge coefficients of flow nozzles

Date: April 1955
Creator: Simmons, Frederick S
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Analytical determination of effect of water injection on power output of turbine-propeller engine

Analytical determination of effect of water injection on power output of turbine-propeller engine

Date: March 1955
Creator: Ross, Albert O & Huppert, Merle C
Description: None
Contributing Partner: UNT Libraries Government Documents Department
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