The Making of a General :  William Tecumseh Sherman and the Art of War

The Making of a General : William Tecumseh Sherman and the Art of War

Date: January 1965
Creator: Vetter, Charles E.
Description: This thesis is an attempt to trace this evolution which led Sherman to be designated as the first modern general.
Contributing Partner: UNT Libraries
The Yucca, Yearbook of North Texas State College, 1961

The Yucca, Yearbook of North Texas State College, 1961

Date: 1961
Creator: North Texas State College
Description: Yearbook for North Texas State College in Denton, Texas includes photos of and information about the school, student body, professors, and organizations. Indexes start on page 512.
Contributing Partner: UNT Libraries Special Collections
Analysis of a Pneumatic Probe for Measuring Exhaust-Gas Temperatures with Some Preliminary Experimental Results

Analysis of a Pneumatic Probe for Measuring Exhaust-Gas Temperatures with Some Preliminary Experimental Results

Date: May 21, 1952
Creator: Scadron, Marvin D.
Description: A pneumatic probe based on continuity of mass flow through two restrictions separated by a cooling chamber was constructed to measure gas temperature at and beyond the limit of thermocouples. This probe consisted of a subsonic flat-plate orifice for the first restriction and a sonic-flow converging-diverging nozzle for the second restriction. The effect of variation in gas constants on the calibration is examined for common engine-exhaust gases. A high-temperature wind tunnel that allowed calibration of the probe at temperatures up to 2000 deg R and. Mach numbers up to 0.8 is described. Agreement to better than 30 deg R between pneumatic probe indication and the indication of a rake of radiation shielded thermocouples indicates that extrapolation of the calibration to higher temperatures is possible with fair accuracy.
Contributing Partner: UNT Libraries Government Documents Department
Experimental investigation of air-cooled turbine blades in turbojet engine.  2:  Rotor blades with 15 fins in cooling-air passages

Experimental investigation of air-cooled turbine blades in turbojet engine. 2: Rotor blades with 15 fins in cooling-air passages

Date: August 1, 1950
Creator: Hickel, R. O. & Ellerbrock, H. H., Jr.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Experimental investigation of air-cooled turbine blades in turbojet engine.  1:  Rotor blades with 10 tubes in cooling-air passages

Experimental investigation of air-cooled turbine blades in turbojet engine. 1: Rotor blades with 10 tubes in cooling-air passages

Date: July 30, 1950
Creator: Ellerbrock, H. H., Jr. & Stepka, F. S.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Interpretation of boundary-layer pressure-rake data in flow with a detached shock

Interpretation of boundary-layer pressure-rake data in flow with a detached shock

Date: August 24, 1950
Creator: Luidens, R. W. & Madden, R. T.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Investigation at Mach number 1.91 of spreading characteristics of jet expanding from choked nozzles

Investigation at Mach number 1.91 of spreading characteristics of jet expanding from choked nozzles

Date: February 11, 1952
Creator: Rousso, M. D. & Baughman, L. E.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Measurement and analysis of turbulent flow containing periodic flow fluctuations

Measurement and analysis of turbulent flow containing periodic flow fluctuations

Date: August 19, 1953
Creator: Mickelsen, W. R. & Laurence, J. C.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Investigations of slot configurations for film-cooled turbine blades by flow visualization methods

Investigations of slot configurations for film-cooled turbine blades by flow visualization methods

Date: October 10, 1950
Creator: Eckert, E. R. G.; Jackson, T. W. & Francisco, A. C.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Some notes on the probable damage to an intercontinental-ballistic-missile warhead following puncture of the heat shield

Some notes on the probable damage to an intercontinental-ballistic-missile warhead following puncture of the heat shield

Date: September 28, 1958
Creator: Strass, H. K. & Goodman, V. M.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
NACA Conference on Aerodynamics of High Speed Aircraft

NACA Conference on Aerodynamics of High Speed Aircraft

Date: November 1, 1955
Creator: unknown
Description: This document contains reproductions of technical papers presented by staff members of the NACA Laboratories at the NACA Conference on Aerodynamics of High-Speed Aircraft held at the Langley Aeronautical Laboratory November 1, 2, and 3, 1955. The primary purpose of the conference was to convey to contractors of the military services and others concerned with the design of aircraft the results of recent research and to provide those attending with an opportunity to discuss these results. The papers in this document are in the same form in which they were orally presented at the conference to facilitate their prompt distribution. The original presentation and this record are considered as complementary to, rather than as substitutes for, the Committee's more complete and formal reports.
Contributing Partner: UNT Libraries Government Documents Department
Investigation of Ejection Releases of an MB-1 Rocket from a 0.04956-Scaled Model of the Convair F-106A Airplane at Several Mach Numbers and Simulated Altitudes

Investigation of Ejection Releases of an MB-1 Rocket from a 0.04956-Scaled Model of the Convair F-106A Airplane at Several Mach Numbers and Simulated Altitudes

Date: August 22, 1957
Creator: Lee, J. B. & Basford, R. C.
Description: As a continuation of an investigation of the ejection release characteristics of an internally carried MB-1 rocket in the Convair F-106A airplane, fin modifications at additional Mach numbers and simulated altitudes have been studied in the 27- by 27-inch preflight jet of the Langley Pilotless Aircraft Research Station at Wallops Island, Va. The MB-1 rocket was ejected with fins open, fins closed, fins closed with a shroud around the fins, and fins folded with a "boattail" placed in between the fins. Dynamically scaled models (0.0^956 scale) were tested at simulated altitudes of 12,000, 18,850, and 27,500 feet at subsonic Mach numbers and at 18,850, 27,500, and 40,000 feet for Mach numbers of 1-39, 1-59, and 1.98. Successful ejections can be obtained for over 10 store diameters from release point by the use of a shroud around the folded fins with the proper ejection velocity and nose-down pitching moment at release. In one case investigated it was found desirable to close off the front one-third of the bomb bay. It appeared that the fins should be opened after release and within 5 "to 6 rocket diameters if no modifications are made on the rocket. An increase in fuselage angle of attack ...
Contributing Partner: UNT Libraries Government Documents Department
Relation of turbojet propulsion system development to the strategic bomber mission

Relation of turbojet propulsion system development to the strategic bomber mission

Date: August 15, 1956
Creator: Rothrock, A. M.; Cesaro, R. S. & Walker, C. L.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
NACA Conference on engine stall and surge

NACA Conference on engine stall and surge

Date: February 3, 1955
Creator: unknown
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Large-scale wind-tunnel tests of an airplane model with a 45 deg sweptback wing of aspect ratio 2.8 with area suction applied to trailing-edge flaps and with several wing leading-edge modifications

Large-scale wind-tunnel tests of an airplane model with a 45 deg sweptback wing of aspect ratio 2.8 with area suction applied to trailing-edge flaps and with several wing leading-edge modifications

Date: November 2, 1956
Creator: Koenig, D. G. & Aoyagi, K.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Preliminary evaluation of the wing leading edge as a missile-mounting location

Preliminary evaluation of the wing leading edge as a missile-mounting location

Date: January 16, 1957
Creator: Hill, P. R. & Hoffman, S.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Preliminary investigation of reflections of  oblique waves from a porous wall

Preliminary investigation of reflections of oblique waves from a porous wall

Date: November 9, 1950
Creator: Davis, D. D., Jr. & Wood, G. P.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Investigation of Ejection Releases of an MB-1 Rocket from a 0.04956-Scaled Model of the Convair F-106A Airplane at Mach Number 1.59

Investigation of Ejection Releases of an MB-1 Rocket from a 0.04956-Scaled Model of the Convair F-106A Airplane at Mach Number 1.59

Date: April 15, 1957
Creator: Lee, J. B.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Analysis of rocket, ramjet, and turbojet engines for supersonic propulsion of long-range missiles.  3:  Ramjet engine performance

Analysis of rocket, ramjet, and turbojet engines for supersonic propulsion of long-range missiles. 3: Ramjet engine performance

Date: August 5, 1954
Creator: Weber, R. J. & Luidens, R. W.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Analysis of rocket, ramjet, turbojet engines for supersonic propulsion of long-range missiles.  2:  Rocket missile performance

Analysis of rocket, ramjet, turbojet engines for supersonic propulsion of long-range missiles. 2: Rocket missile performance

Date: October 11, 1954
Creator: Huff, V. N. & Kerrebrock, J.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Analysis of the liquid-metal turbojet cycle for propulsion of nuclear powered aircraft

Analysis of the liquid-metal turbojet cycle for propulsion of nuclear powered aircraft

Date: November 19, 1951
Creator: Wachtl, W. W. & Rom, F. E.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Analytical determination of local surface heat-transfer coefficients for cooled turbine blades from measured metal temperatures

Analytical determination of local surface heat-transfer coefficients for cooled turbine blades from measured metal temperatures

Date: April 10, 1950
Creator: Brown, W. B. & Esgar, J. B.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Analysis of heat transfer and fluid friction for fully developed turbulent flow of supercritical water with variable fluid properties in a smooth tube

Analysis of heat transfer and fluid friction for fully developed turbulent flow of supercritical water with variable fluid properties in a smooth tube

Date: January 30, 1953
Creator: Deissler, R. G. & Taylor, M. F.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Comparison of various heat exchangers for liquid-metal nuclear turbojet over range of flight and operating conditions

Comparison of various heat exchangers for liquid-metal nuclear turbojet over range of flight and operating conditions

Date: April 28, 1958
Creator: Ragsdale, R. G.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
FIRST PREV 1 2 NEXT LAST