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  Partner: UNT Libraries Government Documents Department
 Serial/Series Title: NACA Memorandum Report
 Collection: Technical Report Archive and Image Library
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
Correlation of wind-tunnel predictions with flight tests of a twin-engine airplane I : longitudinal-stability and -control characteristics

Correlation of wind-tunnel predictions with flight tests of a twin-engine airplane I : longitudinal-stability and -control characteristics

Date: April 4, 1945
Creator: Kauffman, William M
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Static-Thrust Investigation of Full-Scale PV-2 Helicopter Rotors Having NACA 0012.6 and 23012.6 Airfoil Sections

Static-Thrust Investigation of Full-Scale PV-2 Helicopter Rotors Having NACA 0012.6 and 23012.6 Airfoil Sections

Date: May 1, 1946
Creator: Lipson, Stanley
Description: An investigation was conducted to compare the performance of two 25-ft-diam rotors which had identical dimensions and were similar in construction but different in blade airfoil-sections. Tests were conducted at indicated blade pitch angles from 3 degrees to 11.5 degrees and rotor speeds of 200, 290, and 371 rpm. The 23012.6 rotor required 2 percent less power to hover than the 0012.6. At thrust coefficients above design, the performance of the 23012.6 became better than the 0012.6 rotor.
Contributing Partner: UNT Libraries Government Documents Department
High-speed photographs of a YR-4B production rotor blade for simulated flight conditions in the Langley full-scale tunnel

High-speed photographs of a YR-4B production rotor blade for simulated flight conditions in the Langley full-scale tunnel

Date: March 1, 1945
Creator: Schaefer, Raymond F
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Full-scale-tunnel performance tests of the PV-2 helicopter rotor

Full-scale-tunnel performance tests of the PV-2 helicopter rotor

Date: April 1, 1945
Creator: Migotsky, Eugene
Description: None
Contributing Partner: UNT Libraries Government Documents Department
A preliminary theoretical study of helicopter-blade flutter involving dependence upon coning angle and pitch setting

A preliminary theoretical study of helicopter-blade flutter involving dependence upon coning angle and pitch setting

Date: July 1, 1946
Creator: Coleman, Robert P
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Spray characteristics and take-off and landing stability of several modifications of a 1/8-size model of the PBN-1 flying boat : NACA model 192

Spray characteristics and take-off and landing stability of several modifications of a 1/8-size model of the PBN-1 flying boat : NACA model 192

Date: April 1, 1945
Creator: Zeck, Howard
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Nitrous oxide supercharging of an aircraft-engine cylinder

Nitrous oxide supercharging of an aircraft-engine cylinder

Date: June 1, 1945
Creator: Huppert, Merle C
Description: None
Contributing Partner: UNT Libraries Government Documents Department