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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
Date: May 1, 1946
Creator: Weil, Joseph
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Permallink:digital.library.unt.edu/ark:/67531/metadc60945/
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
Permallink:digital.library.unt.edu/ark:/67531/metadc61848/
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
Permallink:digital.library.unt.edu/ark:/67531/metadc61233/
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
Permallink:digital.library.unt.edu/ark:/67531/metadc62035/
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
Permallink:digital.library.unt.edu/ark:/67531/metadc62312/
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
Permallink:digital.library.unt.edu/ark:/67531/metadc61813/
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
Permallink:digital.library.unt.edu/ark:/67531/metadc61964/
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
Permallink:digital.library.unt.edu/ark:/67531/metadc61218/
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
Permallink:digital.library.unt.edu/ark:/67531/metadc61183/
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
Permallink:digital.library.unt.edu/ark:/67531/metadc62408/