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  Partner: UNT Libraries Government Documents Department
 Serial/Series Title: NACA Memorandum Report
 Collection: National Advisory Committee for Aeronautics Collection
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
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 wind-tunnel tests of a twin-fuselage pursuit airplane

High-speed wind-tunnel tests of a twin-fuselage pursuit airplane

Date: April 24, 1946
Creator: Tkac, Victor B
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Tests of cast aluminum-alloy mixed-flow impellers

Tests of cast aluminum-alloy mixed-flow impellers

Date: April 1, 1946
Creator: Schwartz, Irving R
Description: None
Contributing Partner: UNT Libraries Government Documents Department
An evaluation of the knock-limited performance of triptane

An evaluation of the knock-limited performance of triptane

Date: March 1, 1946
Creator: Barnett, Henry C
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Investigation of ice formation in the induction system of an aircraft engine I : ground tests

Investigation of ice formation in the induction system of an aircraft engine I : ground tests

Date: March 1, 1946
Creator: Ellisman, Carl
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Test-stand investigation of cooling characteristics and factors affecting temperature distribution of a double-row aircraft engine

Test-stand investigation of cooling characteristics and factors affecting temperature distribution of a double-row aircraft engine

Date: March 1, 1946
Creator: Jones, Robert J
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Tests of a 1/7-scale powered model of the Kaiser tailless airplane in the Langley full-scale tunnel

Tests of a 1/7-scale powered model of the Kaiser tailless airplane in the Langley full-scale tunnel

Date: March 1, 1946
Creator: Rickey, E A
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Altitude-wind-tunnel tests of power-plant installation in jet-propelled fighter

Altitude-wind-tunnel tests of power-plant installation in jet-propelled fighter

Date: February 1, 1946
Creator: Jagger, James M
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Calibrations of service pitot tubes in the Langley 24-inch high-speed tunnel

Calibrations of service pitot tubes in the Langley 24-inch high-speed tunnel

Date: February 1, 1946
Creator: Lindsey, W F
Description: None
Contributing Partner: UNT Libraries Government Documents Department