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Partner:
UNT Libraries Government Documents Department
Serial/Series Title:
NACA Memorandum Report
Collection:
National Advisory Committee for Aeronautics Collection
The problem of landing
Date: February 1, 1922
Creator: Pistolesi, E
Description: The author discusses various aspects of landing aircraft such as the actual process of touchdown and the problems associated with the tail skid touching the ground before the landing gear.
Contributing Partner: UNT Libraries Government Documents Department
Permallink:digital.library.unt.edu/ark:/67531/metadc53631/
Wind-Tunnel Investigation of Devices for Improving the Diving Characteristics of Airplanes
Date: April 23, 1943
Creator: Erickson, Albert L
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Permallink:digital.library.unt.edu/ark:/67531/metadc61223/
Measurements of the flying qualities of a Bell P-39D-1 airplane (AAF NO. 41-28378)
Date: September 1, 1943
Creator: Hoover, H H
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Permallink:digital.library.unt.edu/ark:/67531/metadc61077/
Ditching tests with a 1/11-size model of the Army B-25 airplane in NACA tank number 2 and on an outdoor catapult
Date: October 1, 1944
Creator: Steiner, Margaret F
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Permallink:digital.library.unt.edu/ark:/67531/metadc62629/
Resume of NACA stability and control tests of the Bell P-63 series airplane
Date: October 1, 1944
Creator: Johnson, Harold I
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Permallink:digital.library.unt.edu/ark:/67531/metadc61079/
Accelerations and bottom pressures measured on a B-24D airplane in a ditching test
Date: November 1, 1944
Creator: Steiner, Margaret F
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Permallink:digital.library.unt.edu/ark:/67531/metadc61135/
Aerodynamic tests of an NACA 66(215)-116, a=0.6 airfoil with a 0.25c slotted flap for the Fleetwings XA-39 airplane
Date: November 1, 1944
Creator: Cahill, Jones F
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Permallink:digital.library.unt.edu/ark:/67531/metadc61411/
Bending and shear stresses developed by the instantaneous arrest of the root of a cantilever beam with a mass at its tip
Date: November 1, 1944
Creator: Schmieder, Albert K
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Permallink:digital.library.unt.edu/ark:/67531/metadc62215/
Ditching tests with a 1/10-size model of the Army A-20A airplane in Langley tank no.2 and on an outdoor catapult
Date: November 1, 1944
Creator: Steiner, Margaret F
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Permallink:digital.library.unt.edu/ark:/67531/metadc62621/
Estimates of the vertical-tail loads of a Bell P-63A-1 airplane (AAF No. 42-68889) in accelerated rolling maneuvers based on flight tests with two vertical-tail arrangements
Date: November 1, 1944
Creator: Johnson, Harold I
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Permallink:digital.library.unt.edu/ark:/67531/metadc61501/