You limited your search to:

 Serial/Series Title: NACA Advanced Restricted Reports
 Collection: Technical Report Archive and Image Library
Additional design charts relating to the stalling of tapered wings

Additional design charts relating to the stalling of tapered wings

Date: January 1943
Creator: Harmon, Sidney M
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Aerodynamic characteristics and flap loads of perforated double split flaps on a rectangular NACA 23012 airfoil

Aerodynamic characteristics and flap loads of perforated double split flaps on a rectangular NACA 23012 airfoil

Date: January 1943
Creator: Turner, Thomas R
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Aerodynamic factors affecting the ability of a pilot to return an airplane to level from a banked attitude by use of the rudder alone and without change of heading

Aerodynamic factors affecting the ability of a pilot to return an airplane to level from a banked attitude by use of the rudder alone and without change of heading

Date: October 1941
Creator: Harmon, S M
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Altitude rating of electrical apparatus

Altitude rating of electrical apparatus

Date: January 1943
Creator: Lebenbaum, Paul, Jr
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Aluminum-zinc-magnesium-copper casting alloys

Aluminum-zinc-magnesium-copper casting alloys

Date: July 1941
Creator: Kempf, L. W.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Analysis of Effect of Rolling Pull-Outs on Wing and Aileron Loads of a Fighter Airplane

Analysis of Effect of Rolling Pull-Outs on Wing and Aileron Loads of a Fighter Airplane

Date: March 1946
Creator: Pearson, Henry A. & Aiken, William S.
Description: An analysis was made to determine the effect of rolling pull-out maneuvers on the wing and aileron loads of a typical fighter airplane, the P-47B. The results obtained indicate that higher loads are imposed upon wings and ailerons because of the rolling pull-out maneuver, than would be obtained by application of the loading requirements to which the airplane was designed. An increase of 102 lb or 15 percent of wing weight would be required if the wing were designed for rolling pull-out maneuver. It was also determined that the requirements by which the aileron was originally designed were inadequate.
Contributing Partner: UNT Libraries Government Documents Department
The analysis of strains indicated by multiple-strand resistance-type wire strain gages used as rosettes

The analysis of strains indicated by multiple-strand resistance-type wire strain gages used as rosettes

Date: January 1, 1943
Creator: Dow, Norris F
Description: None
Contributing Partner: UNT Libraries Government Documents Department
An analysis of the effect of core structure and performance on volume and shape of cross-flow tubular intercoolers

An analysis of the effect of core structure and performance on volume and shape of cross-flow tubular intercoolers

Date: December 1942
Creator: Valerino, Michael F
Description: None
Contributing Partner: UNT Libraries Government Documents Department
An analytical study of wing and tail loads associated with an elevator deflection

An analytical study of wing and tail loads associated with an elevator deflection

Date: June 1, 1941
Creator: Garvin, J B
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Calculated effects of full-span slotted and Fowler flaps on longitudinal stability and control characteristics for a typical fighter-type airplane with various tail modifications

Calculated effects of full-span slotted and Fowler flaps on longitudinal stability and control characteristics for a typical fighter-type airplane with various tail modifications

Date: July 1, 1942
Creator: Goranson, R Fabian
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Calibration of three temperature probes and a pressure probe at high speeds

Calibration of three temperature probes and a pressure probe at high speeds

Date: April 1, 1942
Creator: Lindsey, W F
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Characteristics of beveled-trailing-edge elevators on a typical pursuit fuselage at altitudes simulating-normal flight and spin conditions

Characteristics of beveled-trailing-edge elevators on a typical pursuit fuselage at altitudes simulating-normal flight and spin conditions

Date: December 1, 1942
Creator: Gillis, Clarence L
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Characteristics of plain and balanced elevators on a typical pursuit fuselage at attitudes simulating normal-flight and spin conditions

Characteristics of plain and balanced elevators on a typical pursuit fuselage at attitudes simulating normal-flight and spin conditions

Date: March 1, 1942
Creator: Hoggard, H Page, Jr
Description: None
Contributing Partner: UNT Libraries Government Documents Department
The Characteristics of Two Model Six-Blade Counterrotating Pusher Propellers of Conventional and Improved Aerodynamic Design

The Characteristics of Two Model Six-Blade Counterrotating Pusher Propellers of Conventional and Improved Aerodynamic Design

Date: April 1, 1942
Creator: Pepper, Edward & McHugh, James G.
Description: Two airfoil plans were used for propeller blades. One is modified Clark Y section designed for structural reliability and the second an NACA 16 airfoil section designed to produce minimum aerodynamic losses. At low air speeds, the propeller designed for aerodynamic effects showed a gain of from 1.5 to 4.0 percent in propulsive efficiency over the conventional type depending on the pitch. Because of the numerous variables involved, the effect of each one on the aerodynamic characteristics of the propellers could not be isolated.
Contributing Partner: UNT Libraries Government Documents Department
Charts of pressure, density, and temperature changes at an abrupt increase in cross-sectional area of flow of compressible air

Charts of pressure, density, and temperature changes at an abrupt increase in cross-sectional area of flow of compressible air

Date: January 1, 1945
Creator: Joyner, Upshur T
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Comparison of Intercooler Characteristics

Comparison of Intercooler Characteristics

Date: November 1, 1942
Creator: Valerino, Michael F
Description: No abstract available.
Contributing Partner: UNT Libraries Government Documents Department
Comparison of various methods for computing drag from wake surveys

Comparison of various methods for computing drag from wake surveys

Date: January 1, 1943
Creator: Davis, Wallace F
Description: None
Contributing Partner: UNT Libraries Government Documents Department
A correlation of the dimensions, proportions, and loadings of existing seaplane floats and flying boat hulls

A correlation of the dimensions, proportions, and loadings of existing seaplane floats and flying boat hulls

Date: March 1943
Creator: Locke, Fred W S , Jr
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Critical speeds and profile drag of the inboard sections of a conventional propeller

Critical speeds and profile drag of the inboard sections of a conventional propeller

Date: September 1, 1941
Creator: Luoma, Arvo A
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Determination of the stability and control characteristics of airplanes from tests of powered models

Determination of the stability and control characteristics of airplanes from tests of powered models

Date: July 1, 1942
Creator: Swanson, Robert S
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Development of Cowling for Long-Nose Air-Cooled Engine in the NACA Full-Scale Wind Tunnel

Development of Cowling for Long-Nose Air-Cooled Engine in the NACA Full-Scale Wind Tunnel

Date: October 1, 1941
Creator: Guryansky, Eugene R. & Silverstein, Abe
Description: An investigation of cowlings for long-nose radial engines was made on the Curtiss XP-42 fighter in the NACA full-scale wind tunnel. The unsatisfactory aerodynamic characteristics of all the cowlings with scoop inlets tested led to the development of the annular high-velocity inlet cowlings. Tests showed that ratio of cooling-air velocity at cowling inlet to stream velocity should not be less than 0.5 for this type of cowling and that critical compressibility speed can be extended to more than 500 mph at 20,000 ft altitude.
Contributing Partner: UNT Libraries Government Documents Department
Dynamic stress calculations for two airplanes in various gusts

Dynamic stress calculations for two airplanes in various gusts

Date: September 1, 1941
Creator: Pierce, Harold B
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Effect of additions of aromatics on the knocking characteristics of several 100-octane fuels at two engine speeds

Effect of additions of aromatics on the knocking characteristics of several 100-octane fuels at two engine speeds

Date: May 1, 1942
Creator: Harries, Myron L
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Effect of an aromatic mixture added to two 100-octane fuels on engine temperatures and fuel consumption

Effect of an aromatic mixture added to two 100-octane fuels on engine temperatures and fuel consumption

Date: June 1, 1942
Creator: Jones, Anthony W
Description: None
Contributing Partner: UNT Libraries Government Documents Department
FIRST PREV 1 2 3 4 5 NEXT LAST