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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 1, 1955
Creator: Beckwith, Ivan E
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Acoustic analysis of ram-jet buzz

Acoustic analysis of ram-jet buzz

Date: November 1, 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 1, 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 1, 1955
Creator: Beranek, Leo L
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 1, 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 1, 1955
Creator: Critzos, Chris C
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 1, 1955
Creator: Daley, Bernard N
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 1, 1955
Creator: Martin, John C
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
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
Description: None
Contributing Partner: UNT Libraries Government Documents Department
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