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  Partner: UNT Libraries Government Documents Department
 Collection: Technical Report Archive and Image Library
Theoretical distribution of lift on thin wings at supersonic speeds : (an extension)

Theoretical distribution of lift on thin wings at supersonic speeds : (an extension)

Date: May 1, 1948
Creator: Evvard, John C
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Theoretical distribution of load over a swept-back wing

Theoretical distribution of load over a swept-back wing

Date: October 1, 1942
Creator: Cohen, Doris
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Theoretical distribution of slip angles in an aggregate of face-centered cubic crystals

Theoretical distribution of slip angles in an aggregate of face-centered cubic crystals

Date: August 1, 1952
Creator: Hedgepeth, John M
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Theoretical effect of inlet hub-tip-radius ratio and design specific mass flow on design performance of axial-flow compressors

Theoretical effect of inlet hub-tip-radius ratio and design specific mass flow on design performance of axial-flow compressors

Date: April 1, 1950
Creator: Wu, Chung-Hua
Description: None
Contributing Partner: UNT Libraries Government Documents Department
A theoretical estimate of the effects of compressibility on the performance of a helicopter rotor in various flight conditions

A theoretical estimate of the effects of compressibility on the performance of a helicopter rotor in various flight conditions

Date: October 1, 1956
Creator: Gessow, Alfred
Description: The effects of compressibility arising from high-tip-speed operation on the flapping, thrust, and power of a helicopter rotor in forward speed are investigated for a particular set of airfoil characteristics. Tip-speed ratios ranging from 0.2 to 0.5 were covered at several tip-speed values.
Contributing Partner: UNT Libraries Government Documents Department
Theoretical Evaluation of Methods of Cooling the Blades of Gas Turbines

Theoretical Evaluation of Methods of Cooling the Blades of Gas Turbines

Date: February 11, 1947
Creator: Sanders, J. C.
Description: A study was made of heat transfer in turbine blades and the effects on blade temperature of cooling the blade root and tip, changing the dimensions of the blades, raising the cycle temperatures, insulating with ceramics, and cooling by circulation of air or water through hollow blades.
Contributing Partner: UNT Libraries Government Documents Department
Theoretical evaluation of the ducted-fan turbojet engine

Theoretical evaluation of the ducted-fan turbojet engine

Date: November 1, 1948
Creator: Parisen, Richard B
Description: None
Contributing Partner: UNT Libraries Government Documents Department
The theoretical flow of a frictionless, adiabatic, perfect gas inside of a two-dimensional hyperbolic nozzle

The theoretical flow of a frictionless, adiabatic, perfect gas inside of a two-dimensional hyperbolic nozzle

Date: May 1, 1946
Creator: Emmons, Howard W
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Theoretical force and moments due to sideslip of a number of vertical tail configurations at supersonic speeds

Theoretical force and moments due to sideslip of a number of vertical tail configurations at supersonic speeds

Date: September 1, 1951
Creator: Martin, John C
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Theoretical investigation and application of transonic similarity law for two dimensional flow

Theoretical investigation and application of transonic similarity law for two dimensional flow

Date: October 1, 1950
Creator: Perl, William
Description: None
Contributing Partner: UNT Libraries Government Documents Department