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  Partner: UNT Libraries Government Documents Department
 Decade: 1950-1959
 Serial/Series Title: NACA Technical Notes
 Collection: National Advisory Committee for Aeronautics Collection
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
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
An air-flow-direction pickup suitable for telemetering use on pilotless aircraft

An air-flow-direction pickup suitable for telemetering use on pilotless aircraft

Date: October 1, 1956
Creator: Ikard, Wallace L
Description: A vane-type air-flow-direction pickup is described which is suitable for telemetering angle-of-attack and angle-of-sideslip data from rocket-propelled pilotless aircraft models. Test results which are presented show that the device performs well under high accelerations and is stable throughout a Mach number rage from subsonic to above a Mach number of 2.5.
Contributing Partner: UNT Libraries Government Documents Department
Air forces and moments on triangular and related wings with subsonic leading edges oscillating in supersonic potential flow

Air forces and moments on triangular and related wings with subsonic leading edges oscillating in supersonic potential flow

Date: September 1, 1951
Creator: Watkins, Charles E
Description: None
Contributing Partner: UNT Libraries Government Documents Department
An airborne indicator for measuring vertical velocity of airplanes at wheel contact

An airborne indicator for measuring vertical velocity of airplanes at wheel contact

Date: February 1, 1953
Creator: Dreher, Robert C
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Airfoil profiles for minimum pressure drag at supersonic velocities : application of shock-expansion theory, including consideration of hypersonic range

Airfoil profiles for minimum pressure drag at supersonic velocities : application of shock-expansion theory, including consideration of hypersonic range

Date: September 17, 1952
Creator: Chapman, Dean R
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
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
Analogue-computer simulation of an autopilot servo system having nonlinear response characteristics

Analogue-computer simulation of an autopilot servo system having nonlinear response characteristics

Date: June 1, 1952
Creator: Jones, Arthur L
Description: None
Contributing Partner: UNT Libraries Government Documents Department