The effects of extensible rocket racks on lift, drag, and stability of a 1/10-scale rocket-boosted model of the McDonnell XF3H-1 airplane for a Mach number range of 0.60 to 1.34 : TED No. NACA DE 31

The effects of extensible rocket racks on lift, drag, and stability of a 1/10-scale rocket-boosted model of the McDonnell XF3H-1 airplane for a Mach number range of 0.60 to 1.34 : TED No. NACA DE 31

Date: June 16, 1953
Creator: Crabill, Norman L
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Stability and control flight tests of a 0.13-scale model of the consolidated-Vultee XFY-1 airplane in take-offs, landings, and hovering flight : TED No. NACA DE 368

Stability and control flight tests of a 0.13-scale model of the consolidated-Vultee XFY-1 airplane in take-offs, landings, and hovering flight : TED No. NACA DE 368

Date: October 1, 1952
Creator: Lovell, Powell M., Jr.; Smith, Charles C., Jr. & Kirby, Robert H.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
An investigation of the low-speed stability and control characteristics of a 1/10-scale model of the McDonnell XF3H-1 airplane : TED No. NACA DE 344

An investigation of the low-speed stability and control characteristics of a 1/10-scale model of the McDonnell XF3H-1 airplane : TED No. NACA DE 344

Date: October 11, 1951
Creator: Draper, John W
Description: At the request of the Bureau of Aeronautics, Navy Department, an investigation of the low-speed, power-off stability and control characteristics of a 1/10-scale model of the McDonnell XF3H-1 airplane has been made in the Langley free-flight tunnel. Flight tests of the model in the clean and in the slats-and-flaps-extended conditions were made over a lift-coefficient range from about 0.5 through the stall. Only low-altitude conditions were simulated and no attempt was made to determine the effect on the stability characteristics of freeing the controls. Static force tests were made to determine the static longitudinal and lateral stability derivatives and rotary force tests were made to determine the dynamic rolling derivatives. Calculations were also made to determine the damping of the lateral oscillation for correlation with the flight results.
Contributing Partner: UNT Libraries Government Documents Department
Free-flight tests of three 1/9-scale models of the wing-ram-jet configuration of the Grumman XSSM-N-6A (Rigel) missile to investigate the possibility of flutter : TED No. NACA DE 223

Free-flight tests of three 1/9-scale models of the wing-ram-jet configuration of the Grumman XSSM-N-6A (Rigel) missile to investigate the possibility of flutter : TED No. NACA DE 223

Date: April 14, 1953
Creator: O'Kelly, Burke R & Lauten, William T , Jr
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Free-spinning-tunnel investigation of a 1/30-scale model of the Grumman XS2F-1 airplane : TED No. NACA DE 366

Free-spinning-tunnel investigation of a 1/30-scale model of the Grumman XS2F-1 airplane : TED No. NACA DE 366

Date: September 17, 1952
Creator: Healy, Frederick M
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Free-spinning tunnel investigation of a 1/20-scale model of the     McDonnell F2H-3 airplane

Free-spinning tunnel investigation of a 1/20-scale model of the McDonnell F2H-3 airplane

Date: July 24, 1951
Creator: Wilson, Jack H
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Wind-tunnel investigation of the motion of a 1/10-scale model of the Douglas XF4D-1 escape capsule when jettisoned by jet ejection : TED No. NACA DE 359

Wind-tunnel investigation of the motion of a 1/10-scale model of the Douglas XF4D-1 escape capsule when jettisoned by jet ejection : TED No. NACA DE 359

Date: October 7, 1953
Creator: Jshnson, Harold, S
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Supplementary free-spinning-tunnel investigation of a 1/20-scale model of the McDonnell F2H-3 airplane with external stores installed : TED No. NACA DE 2393

Supplementary free-spinning-tunnel investigation of a 1/20-scale model of the McDonnell F2H-3 airplane with external stores installed : TED No. NACA DE 2393

Date: June 9, 1952
Creator: Wilson, Jack H
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Free-spinning-tunnel investigation to determine the effect of two nose designs on spin and recovery characteristics of a 1/20-scale model of the McDonnel XF3H-1 airplane : TED No. NACA DE 343

Free-spinning-tunnel investigation to determine the effect of two nose designs on spin and recovery characteristics of a 1/20-scale model of the McDonnel XF3H-1 airplane : TED No. NACA DE 343

Date: August 17, 1951
Creator: Wilson, Jack H
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Hydrodynamic investigation of a 1/13-scale model of the consolidated vultee skate 7 seaplane equipped with twin hydro-skis : TED No. NACA DE 342

Hydrodynamic investigation of a 1/13-scale model of the consolidated vultee skate 7 seaplane equipped with twin hydro-skis : TED No. NACA DE 342

Date: November 7, 1951
Creator: Mckann, Robert E; Coffee, Claude W & Arabian, Donald D
Description: None
Contributing Partner: UNT Libraries Government Documents Department
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