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  Partner: UNT Libraries Government Documents Department
 Serial/Series Title: NACA Memorandum Report
An investigation of a thermal ice-prevention system for a C-46 cargo airplane V : effect of thermal system on airplane cruise performance
No Description digital.library.unt.edu/ark:/67531/metadc279663/
Wind-tunnel investigation of the effects of spoilers on the characteristics of a low-drag airfoil equipped with a 0.25-chord slotted flap
No Description digital.library.unt.edu/ark:/67531/metadc279657/
Tests of a thermal ice-prevention system for a wing leading-edge landing-light installation
No Description digital.library.unt.edu/ark:/67531/metadc279556/
Single-cylinder oil-control tests of porous chrome plated cylinder barrels for radial air-cooled engines
No Description digital.library.unt.edu/ark:/67531/metadc279560/
Effect of the performance of a turbosupercharged engine of an exhaust-gas-to-air heat exchanger for thermal ice prevention
No Description digital.library.unt.edu/ark:/67531/metadc279594/
F-3 and F-4 engine tests of several high-antiknock components of aviation fuel
No Description digital.library.unt.edu/ark:/67531/metadc62363/
Charts showing stability and control characteristics of airplanes in flight
No Description digital.library.unt.edu/ark:/67531/metadc60953/
Free-spinning, longitudinal-trim, and tumbling tests of 1/17.8-scale models of the Cornelius XFG-1 glider
No Description digital.library.unt.edu/ark:/67531/metadc60856/
The effect of some design parameters on ditching characteristics
No Description digital.library.unt.edu/ark:/67531/metadc60888/
Langley full-scale-tunnel stability and control tests of the Bell YP-59A airplane
No Description digital.library.unt.edu/ark:/67531/metadc60863/
Performance selection charts for gliders and twin-engine tow planes
No Description digital.library.unt.edu/ark:/67531/metadc60841/
Vibration-response tests of a 1/5-scale model of the Grumman F6F airplane in the Langley 16-foot high-speed tunnel
No Description digital.library.unt.edu/ark:/67531/metadc60875/
Some notes on the effects of jet-exit design on static longitudinal stability
No Description digital.library.unt.edu/ark:/67531/metadc60945/
Correlation of wind-tunnel predictions with flight tests of a twin-engine airplane I : longitudinal-stability and -control characteristics
No Description digital.library.unt.edu/ark:/67531/metadc61036/
Static-Thrust Investigation of Full-Scale PV-2 Helicopter Rotors Having NACA 0012.6 and 23012.6 Airfoil Sections
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. digital.library.unt.edu/ark:/67531/metadc61848/
High-speed photographs of a YR-4B production rotor blade for simulated flight conditions in the Langley full-scale tunnel
No Description digital.library.unt.edu/ark:/67531/metadc61844/
Full-scale-tunnel performance tests of the PV-2 helicopter rotor
No Description digital.library.unt.edu/ark:/67531/metadc61846/
A preliminary theoretical study of helicopter-blade flutter involving dependence upon coning angle and pitch setting
No Description digital.library.unt.edu/ark:/67531/metadc61843/
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
No Description digital.library.unt.edu/ark:/67531/metadc61791/
Nitrous oxide supercharging of an aircraft-engine cylinder
No Description digital.library.unt.edu/ark:/67531/metadc61911/
Effect of engine-operating variables and internal coolants on spark-advance requirements of a liquid-cooled cylinder
No Description digital.library.unt.edu/ark:/67531/metadc61914/
Spin tests of a 0.059-scale model of the Curtiss-Wright XP-55 airplane
No Description digital.library.unt.edu/ark:/67531/metadc61242/
Longitudinal-trim tests of a 0.059-scale model of the Curtiss-Wright XP-55 airplane
No Description digital.library.unt.edu/ark:/67531/metadc61240/
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
No Description digital.library.unt.edu/ark:/67531/metadc61501/
Effect of Mach and Reynolds numbers on the maximum lift coefficient obtainable in gradual and abrupt stalls of a pursuit airplane equipped with a low-drag wing
No Description digital.library.unt.edu/ark:/67531/metadc61288/
Some flight measurements on pressure distribution during tail buffeting
No Description digital.library.unt.edu/ark:/67531/metadc61505/
Flight measurements of the flying qualities of an F6F-3 airplane (BuAer No. 04776) I : longitudinal stability and control
No Description digital.library.unt.edu/ark:/67531/metadc61068/
The effect of the skis on the power-off stability characteristics of a twin-engine cargo airplane
No Description digital.library.unt.edu/ark:/67531/metadc61063/
Correlation of wind-tunnel predictions with flight tests of a twin-engine patrol airplane II : lateral- and directional-stability and control characteristics
No Description digital.library.unt.edu/ark:/67531/metadc61041/
Flight tests of an SB2C-3 airplane with a production and tilted propeller axis
No Description digital.library.unt.edu/ark:/67531/metadc61047/
Measurement of flying qualities of a DeHavilland Mosquito F-8 airplane (AAF No. 43-334960) II : longitudinal stability and control characteristics
No Description digital.library.unt.edu/ark:/67531/metadc61048/
Two-dimensional wind-tunnel investigation of six airfoil sections for the wing of the Vega XP2V-1 airplane
No Description digital.library.unt.edu/ark:/67531/metadc61361/
Measurement of individual aileron hinge moments and aileron control characteristics of a P-40F airplane
No Description digital.library.unt.edu/ark:/67531/metadc61642/
Two-dimensional wind-tunnel investigation of spoiler aileron flap model for the Hughes XF-11 airplane
No Description digital.library.unt.edu/ark:/67531/metadc61641/
Estimation of the performance and longitudinal stability and control of a lifting-body type of cargo airplane from tests of simplified models
No Description digital.library.unt.edu/ark:/67531/metadc61179/
Measurement of flying qualities of a Douglas A-26B airplane (AAF No. 41-39120) III : stalling characteristics
No Description digital.library.unt.edu/ark:/67531/metadc61055/
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
No Description digital.library.unt.edu/ark:/67531/metadc61057/
Measurement of flying qualities of a Douglas A-26B airplane (AAF No. 41-39120) I : longitudinal stability and control characteristics
No Description digital.library.unt.edu/ark:/67531/metadc61050/
Measurement of flying qualities of a Douglas A-26B airplane (AAF No. 41-39120) II : lateral and directional stability and control characteristics
No Description digital.library.unt.edu/ark:/67531/metadc61054/
Comparison of predicted and actual control-fixed stability and control characteristics of a Douglas A-26B airplane
No Description digital.library.unt.edu/ark:/67531/metadc61056/
Two-dimensional wind-tunnel investigation of two NACA low-drag airfoil sections equipped with slotted flaps and a plain NACA low-drag airfoil section for XF6U-l airplane
No Description digital.library.unt.edu/ark:/67531/metadc61393/
Analytical investigation of the stability of an F8F dropping model with automatic stabilization
No Description digital.library.unt.edu/ark:/67531/metadc61655/
Two-dimensional wind-tunnel investigation of 0.20-airfoil-chord plain ailerons of different contour on an NACA 65(sub 1)-210 airfoil section
No Description digital.library.unt.edu/ark:/67531/metadc61394/
High-speed wind-tunnel tests of a twin-fuselage pursuit airplane
No Description digital.library.unt.edu/ark:/67531/metadc61233/
The effect of Mach number on the aerodynamic characteristics of a single-engine pursuit airplane as determined from tests of a 1/3-scale model
No Description digital.library.unt.edu/ark:/67531/metadc61229/
Wind-Tunnel Investigation of Devices for Improving the Diving Characteristics of Airplanes
No Description digital.library.unt.edu/ark:/67531/metadc61223/
An estimate of the effect of engine supercharging on the take-off thrust of a typical helicopter at different altitudes and temperatures
No Description digital.library.unt.edu/ark:/67531/metadc61867/
Efficiency of a radial-flow exhaust-gas turbosupercharger turbine with a 12.75-inch tip diameter
No Description digital.library.unt.edu/ark:/67531/metadc61860/
Determination of air-consumption parameters for two radial aircraft engines
No Description digital.library.unt.edu/ark:/67531/metadc61869/
Flight tests of the Sikorsky HNS-1 (Army YR-4B) helicopter II : hovering and vertical-flight performance with the original and an alternate set of main-rotor blades, including a comparison with hovering performance theory
No Description digital.library.unt.edu/ark:/67531/metadc61839/
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