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  Partner: UNT Libraries Government Documents Department
 Serial/Series Title: NACA Wartime Reports
 Collection: National Advisory Committee for Aeronautics Collection
Analysis of a thermal ice-prevention system for wing leading-edge landing-light installations

Analysis of a thermal ice-prevention system for wing leading-edge landing-light installations

Date: January 1, 1944
Creator: Hillendahl, Wesley H
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Analysis of available data on control surfaces having plain-overhang and Frise balances

Analysis of available data on control surfaces having plain-overhang and Frise balances

Date: May 1944
Creator: Toll, Thomas A
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Analysis of available data on the effectiveness of ailerons without exposed overhang balance

Analysis of available data on the effectiveness of ailerons without exposed overhang balance

Date: May 1944
Creator: Crandall, Stewart M. & Swanson, Robert S.
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
Analysis of factors affecting net lift increment attainable with trailing-edge split flaps on tailless airplanes

Analysis of factors affecting net lift increment attainable with trailing-edge split flaps on tailless airplanes

Date: September 1944
Creator: Maggin, Bernard
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Analysis of heat and compressibility effects in internal flow systems and high-speed tests of a ram-jet system

Analysis of heat and compressibility effects in internal flow systems and high-speed tests of a ram-jet system

Date: September 1942
Creator: Baals, Donald D
Description: None
Contributing Partner: UNT Libraries Government Documents Department
An analysis of jet-propulsion systems making direct use of the working substance of a thermodynamic cycle

An analysis of jet-propulsion systems making direct use of the working substance of a thermodynamic cycle

Date: February 1, 1945
Creator: Rubert, Kennedy F
Description: None
Contributing Partner: UNT Libraries Government Documents Department
An analysis of life expectancy of airplane wings in normal cruising flight

An analysis of life expectancy of airplane wings in normal cruising flight

Date: July 1, 1945
Creator: Putnam, Abbott A
Description: None
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 analysis of the fatigue life of an airplane wing structure under overload conditions

An analysis of the fatigue life of an airplane wing structure under overload conditions

Date: February 1946
Creator: Reisert, Thomas D
Description: None
Contributing Partner: UNT Libraries Government Documents Department
An analysis of the indications of the University of Chicago airborne turbulence indicator in gusty air

An analysis of the indications of the University of Chicago airborne turbulence indicator in gusty air

Date: August 1946
Creator: Pratt, K G
Description: None
Contributing Partner: UNT Libraries Government Documents Department
An analysis of the skipping characteristics of some full-size flying boats

An analysis of the skipping characteristics of some full-size flying boats

Date: January 1946
Creator: Locke, F. W. S., Jr.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Analysis of V-G Records from the SNB-1 Airplane

Analysis of V-G Records from the SNB-1 Airplane

Date: July 1946
Creator: Meadows, May T. & Walker, Walter G.
Description: Availability data obtained on SNB-1 trainer-class airplanes were analyzed and results presented as flight envelopes which predict occurrences of large values of air speed and acceleration. Comparison is made with SNJ-4 trainer-class airplane data analyzed by the same method. It is concluded that flight envelopes are satisfactory; that the two types show large differences in flight loads and speeds experience; and that SNB-1 will seldom, if ever, exceed design limit load factor and restricted speed, which SNJ-4 can be expected to exceed design-limit load factor and restricted speed in a very small number of flight hours.
Contributing Partner: UNT Libraries Government Documents Department
Analysis of V-G records from the SNJ-4 airplane

Analysis of V-G records from the SNJ-4 airplane

Date: December 1945
Creator: Bennett, S A
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Analysis of vertical-tail loads in rolling pull-out maneuvers

Analysis of vertical-tail loads in rolling pull-out maneuvers

Date: August 1944
Creator: Gilruth, Robert R
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Analysis of wind-tunnel stability and control tests in terms of flying qualities in full-scale airplanes

Analysis of wind-tunnel stability and control tests in terms of flying qualities in full-scale airplanes

Date: October 1943
Creator: Kayten, Gerald G
Description: None
Contributing Partner: UNT Libraries Government Documents Department
An analytical investigation of the effects of elevator-fabric distortion on the longitudinal stability and control of an airplane

An analytical investigation of the effects of elevator-fabric distortion on the longitudinal stability and control of an airplane

Date: May 1, 1944
Creator: Mathews, Charles W
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Analytical investigation of the stability of an F8F dropping model with automatic stabilization

Analytical investigation of the stability of an F8F dropping model with automatic stabilization

Date: December 1, 1945
Creator: Cohen, Doris
Description: None
Contributing Partner: UNT Libraries Government Documents Department
An analytical investigation of thermal-electric means of preventing ice formations on a propeller blade

An analytical investigation of thermal-electric means of preventing ice formations on a propeller blade

Date: August 1, 1944
Creator: Scherrer, Richard
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
Antiknock effectiveness of xylidines in small-scale engines

Antiknock effectiveness of xylidines in small-scale engines

Date: August 1943
Creator: Meyer, Carl L
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Application of a numerical procedure to stress analysis of stringer-reinforced panels

Application of a numerical procedure to stress analysis of stringer-reinforced panels

Date: March 1, 1945
Creator: Kempner, Joseph
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Application of Balancing Tabs to Ailerons

Application of Balancing Tabs to Ailerons

Date: June 1, 1942
Creator: Sears, Richard I.
Description: Analysis was made to determine characteristics required of a balancing-tab system for ailerons in order to reduce aileron stick forces to any desired magnitude. Series of calculations based on section data were made to determine balancing-tab systems of various chord tabs and ailerons that will give, for a particular airplane, zero rate of aileron hinge moment with aileron deflection and yet will produce same maximum rate of roll as a plain unbalanced 15-percent chord aileron of same span. Effects of rolling velocity and of forces in tab link on aileron hinge moments have been included.
Contributing Partner: UNT Libraries Government Documents Department