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  Partner: UNT Libraries Government Documents Department
 Serial/Series Title: NACA Memorandum Report
 Collection: National Advisory Committee for Aeronautics Collection
Flight tests of the high-speed performance of a P-51B airplane (AAF no. 43-12105)

Flight tests of the high-speed performance of a P-51B airplane (AAF no. 43-12105)

Date: December 18, 1944
Creator: Voglewede, T. J. & Danforth, E. C. D.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Power-off tests of the Northrop N9M-2 tailless airplane in the 40- by 80-foot wind tunnel

Power-off tests of the Northrop N9M-2 tailless airplane in the 40- by 80-foot wind tunnel

Date: December 14, 1944
Creator: Stevens, Victor I., Jr. & Mccormack, Gerald M.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
F-3 and F-4 engine tests of several high-antiknock components of aviation fuel

F-3 and F-4 engine tests of several high-antiknock components of aviation fuel

Date: November 1, 1944
Creator: Genco, Russell S
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Charts showing stability and control characteristics of airplanes in flight

Charts showing stability and control characteristics of airplanes in flight

Date: December 1, 1944
Creator: unknown
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Free-spinning, longitudinal-trim, and tumbling tests of 1/17.8-scale models of the Cornelius XFG-1 glider

Free-spinning, longitudinal-trim, and tumbling tests of 1/17.8-scale models of the Cornelius XFG-1 glider

Date: January 1, 1946
Creator: Daughtridge, Lee T , Jr
Description: None
Contributing Partner: UNT Libraries Government Documents Department
The effect of some design parameters on ditching characteristics

The effect of some design parameters on ditching characteristics

Date: July 1, 1945
Creator: Dawson, John R
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Langley full-scale-tunnel stability and control tests of the Bell YP-59A airplane

Langley full-scale-tunnel stability and control tests of the Bell YP-59A airplane

Date: January 1, 1945
Creator: Brewer, Gerald W
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Performance selection charts for gliders and twin-engine tow planes

Performance selection charts for gliders and twin-engine tow planes

Date: May 1, 1945
Creator: Schultz, Wayne F
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Vibration-response tests of a 1/5-scale model of the Grumman F6F airplane in the Langley 16-foot high-speed tunnel

Vibration-response tests of a 1/5-scale model of the Grumman F6F airplane in the Langley 16-foot high-speed tunnel

Date: November 1, 1944
Creator: Regier, Arthur A
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Some notes on the effects of jet-exit design on static longitudinal stability

Some notes on the effects of jet-exit design on static longitudinal stability

Date: May 1, 1946
Creator: Weil, Joseph
Description: None
Contributing Partner: UNT Libraries Government Documents Department
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