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  Partner: UNT Libraries Government Documents Department
 Serial/Series Title: NACA Memorandum Report
 Collection: National Advisory Committee for Aeronautics Collection
Wind-Tunnel Investigation of Devices for Improving the Diving Characteristics of Airplanes

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
Measurements of the flying qualities of a Bell P-39D-1 airplane (AAF NO. 41-28378)

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
Resume of NACA stability and control tests of the Bell P-63 series airplane

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
Bending and shear stresses developed by the instantaneous arrest of the root of a cantilever beam with a mass at its tip

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
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

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
F-3 and F-4 engine tests of several high-antiknock components of aviation fuel

F-3 and F-4 engine tests of several high-antiknock components of aviation fuel

Date: November 1, 1944
Creator: Genco, Russell S
Description: None
Contributing Partner: UNT Libraries Government Documents Department
An investigation of the mutual interference effects of a tail-surface : stern propeller installation on a model simulating the Douglas XB-42 empennage

An investigation of the mutual interference effects of a tail-surface : stern propeller installation on a model simulating the Douglas XB-42 empennage

Date: November 1, 1944
Creator: Marino, Alfred A
Description: None
Contributing Partner: UNT Libraries Government Documents Department
The low-temperature solubility of 24 aromatic amines in aviation gasoline

The low-temperature solubility of 24 aromatic amines in aviation gasoline

Date: November 1, 1944
Creator: Kelly, Richard L
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
Flying qualities of a high-speed bomber with a dual pusher propeller aft of the empennage as estimated from wind-tunnel tests of a 1/8-scale powered model

Flying qualities of a high-speed bomber with a dual pusher propeller aft of the empennage as estimated from wind-tunnel tests of a 1/8-scale powered model

Date: November 4, 1944
Creator: Schnurbusch, Alfred W
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Analysis and correlation of data obtained by six laboratories on fuel-vapor loss from fuel tanks during simulated flight

Analysis and correlation of data obtained by six laboratories on fuel-vapor loss from fuel tanks during simulated flight

Date: December 1, 1944
Creator: Englert, Gerald W
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Charts showing stability and control characteristics of airplanes in flight

Charts showing stability and control characteristics of airplanes in flight

Date: December 1, 1944
Creator: unknown
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Flight and test-stand investigation of high-performance fuels in double-row radial air-cooled engines I : determination of cooling characteristics of flight engine

Flight and test-stand investigation of high-performance fuels in double-row radial air-cooled engines I : determination of cooling characteristics of flight engine

Date: December 1, 1944
Creator: Pragliola, Philip C
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Flight and test-stand investigation of high-performance fuels in double-row radial air-cooled engines II : flight knock data and comparison of fuel knock limits with engine cooling limits in flight

Flight and test-stand investigation of high-performance fuels in double-row radial air-cooled engines II : flight knock data and comparison of fuel knock limits with engine cooling limits in flight

Date: December 1, 1944
Creator: Werner, Milton
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Flight variables affecting fuel-vapor loss from a fuel tank

Flight variables affecting fuel-vapor loss from a fuel tank

Date: December 1, 1944
Creator: Black, Dugald O
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Knock-limited performance of blends of AN-F-28 fuel containing 2 percent aromatic amines IV

Knock-limited performance of blends of AN-F-28 fuel containing 2 percent aromatic amines IV

Date: December 1, 1944
Creator: Tower, Leonard K
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Measurement of flying qualities of a Douglas A-26B airplane (AAF No. 41-39120) I : longitudinal stability and control characteristics

Measurement of flying qualities of a Douglas A-26B airplane (AAF No. 41-39120) I : longitudinal stability and control characteristics

Date: December 1, 1944
Creator: Hoover, H H
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Tests of a thermal ice-prevention system for a wing leading-edge landing-light installation

Tests of a thermal ice-prevention system for a wing leading-edge landing-light installation

Date: December 11, 1944
Creator: Hillendahl, Wesley H
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Power-off tests of the Northrop N9M-2 tailless airplane in the 40- by 80-foot wind tunnel

Power-off tests of the Northrop N9M-2 tailless airplane in the 40- by 80-foot wind tunnel

Date: December 14, 1944
Creator: Stevens, Victor I., Jr. & Mccormack, Gerald M.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Flight tests of the high-speed performance of a P-51B airplane (AAF no. 43-12105)

Flight tests of the high-speed performance of a P-51B airplane (AAF no. 43-12105)

Date: December 18, 1944
Creator: Voglewede, T. J. & Danforth, E. C. D.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
High-speed wind-tunnel tests of semispan horizontal tails with fabric-covered and metal-covered elevators for a bomber airplane

High-speed wind-tunnel tests of semispan horizontal tails with fabric-covered and metal-covered elevators for a bomber airplane

Date: December 18, 1944
Creator: Nelson, Warren H
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Wind Tunnel Investigation of the Effects of Slot Shape and Flap Location on the Characteristics of a Low-Drag Airfoil Equipped with a 0.25-Chord Slotted Flap

Wind Tunnel Investigation of the Effects of Slot Shape and Flap Location on the Characteristics of a Low-Drag Airfoil Equipped with a 0.25-Chord Slotted Flap

Date: December 28, 1944
Creator: Weisman, Yale & Holtzclaw, Ralph W.
Description: Tests were conducted at dynamic pressure of 50 lb per square foot with lift drag and pitch moment measurements throughout useful angle of attack range for constant flap deflection and position of a low-drag airfoil. Two slots were investigated and practical flap paths were selected for each Slot shape had a negligible effect on the maximum lift coefficient flap deflected, the rounded-entry slot had lower profile drag.
Contributing Partner: UNT Libraries Government Documents Department
Correlation of engine-cooling data

Correlation of engine-cooling data

Date: January 1, 1945
Creator: Brevoort, Maurice J
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Langley full-scale-tunnel stability and control tests of the Bell YP-59A airplane

Langley full-scale-tunnel stability and control tests of the Bell YP-59A airplane

Date: January 1, 1945
Creator: Brewer, Gerald W
Description: None
Contributing Partner: UNT Libraries Government Documents Department
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