Experimental investigation of effects of simulated nacelles and wing-root freedoms on supersonic flutter characteristics of a cambered, modified, swept, tapered wing

Experimental investigation of effects of simulated nacelles and wing-root freedoms on supersonic flutter characteristics of a cambered, modified, swept, tapered wing

Date: October 16, 1957
Creator: Hanson, P. W.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Transonic wind-tunnel investigation of static- pressure fluctuations in duct of a scale inlet model of a supersonic fighter-bomber airplane

Transonic wind-tunnel investigation of static- pressure fluctuations in duct of a scale inlet model of a supersonic fighter-bomber airplane

Date: August 6, 1957
Creator: Brooks, J. D.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
A flight and analog study of the effect of elevating the radar-boresight axis upon stability and tracking performance of an automatically controlled interceptor

A flight and analog study of the effect of elevating the radar-boresight axis upon stability and tracking performance of an automatically controlled interceptor

Date: October 16, 1957
Creator: Cheatham, D. C.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Wind-Tunnel Flutter Tests at Mach Numbers up to 3.0 of Boeing Wing Models for Weapons System 110A

Wind-Tunnel Flutter Tests at Mach Numbers up to 3.0 of Boeing Wing Models for Weapons System 110A

Date: September 27, 1957
Creator: Levey, G. M.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
An investigation of ejection releases of submerged and semisubmerged dynamically scaled stores from a simulated bomb bay of a fighter- bomber airplane at supersonic speeds

An investigation of ejection releases of submerged and semisubmerged dynamically scaled stores from a simulated bomb bay of a fighter- bomber airplane at supersonic speeds

Date: December 26, 1956
Creator: Carter, H. S.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Longitudinal aerodynamic characteristics of various configurations of a revised 1/22-scale model of the Republic F-105 airplane at Mach numbers of 1.41 and 2.01

Longitudinal aerodynamic characteristics of various configurations of a revised 1/22-scale model of the Republic F-105 airplane at Mach numbers of 1.41 and 2.01

Date: May 4, 1956
Creator: Foster, G. V.
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
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
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
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