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  Partner: UNT Libraries Government Documents Department
 Serial/Series Title: NACA Research Memorandums
 Collection: Technical Report Archive and Image Library
A method for calculating the lift and center of pressure of wing-body-tail combinations at subsonic, transonic, and supersonic speeds

A method for calculating the lift and center of pressure of wing-body-tail combinations at subsonic, transonic, and supersonic speeds

Date: November 12, 1953
Creator: Nielsen, Jack Norman
Description: None
Contributing Partner: UNT Libraries Government Documents Department
The subsonic lateral and longitudinal static stability characteristics up to large angles of sideslip for a triangular-wing airplane model having a ventral fin

The subsonic lateral and longitudinal static stability characteristics up to large angles of sideslip for a triangular-wing airplane model having a ventral fin

Date: October 25, 1956
Creator: Buell, D. A.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Effects of free-flight rocket-model booster-adapter configurations on the aerodynamic characteristics in pitch and sideslip of a swept-wing fighter airplane model at a Mach number of 2.01

Effects of free-flight rocket-model booster-adapter configurations on the aerodynamic characteristics in pitch and sideslip of a swept-wing fighter airplane model at a Mach number of 2.01

Date: March 25, 1955
Creator: Robinson, R. B.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Effect of throat bleed on the supersonic performance of a half-conical side-inlet system

Effect of throat bleed on the supersonic performance of a half-conical side-inlet system

Date: January 10, 1956
Creator: Mc Kevitt, F. X.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Results of the flight test of a 0.13-scale rocket-boosted model of the McDonnell F4H-1 airplane between Mach numbers of 0.20 and 1.90

Results of the flight test of a 0.13-scale rocket-boosted model of the McDonnell F4H-1 airplane between Mach numbers of 0.20 and 1.90

Date: November 8, 1957
Creator: Dickens, W. L.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Free Spinning and Recovery Characteristics of 1/36-Scale Model of the Republic F-105B Airplane

Free Spinning and Recovery Characteristics of 1/36-Scale Model of the Republic F-105B Airplane

Date: October 9, 1957
Creator: Bowman, James S., Jr.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Experimental Investigation of Flutter and Divergence Characteristics of the Rocket-Motor Fin of the ASROC Missile

Experimental Investigation of Flutter and Divergence Characteristics of the Rocket-Motor Fin of the ASROC Missile

Date: July 31, 1958
Creator: Hanson, P. W.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Investigation of a 1/22-Scale Model of the Republic F-105 Airplane in the Langley 8-Foot Transonic Tunnel Lateral, Directional, and Additional Longitudinal Static Stability and Control

Investigation of a 1/22-Scale Model of the Republic F-105 Airplane in the Langley 8-Foot Transonic Tunnel Lateral, Directional, and Additional Longitudinal Static Stability and Control

Date: August 23, 1957
Creator: Luoma, A. A.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Wind-Tunnel Investigation of the Effect of Spin on the Aerodynamic Characteristics of a 60-Millimeter T-24 Mortar Shell with Several Tail-Fin Configurations

Wind-Tunnel Investigation of the Effect of Spin on the Aerodynamic Characteristics of a 60-Millimeter T-24 Mortar Shell with Several Tail-Fin Configurations

Date: March 21, 1957
Creator: Hayes, W. C., Jr.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Transonic Aerodynamic Characteristics of a 1/15-Scale Model of the Convair B-58 Airplane

Transonic Aerodynamic Characteristics of a 1/15-Scale Model of the Convair B-58 Airplane

Date: October 19, 1956
Creator: Swihart, J. M.
Description: None
Contributing Partner: UNT Libraries Government Documents Department