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  Partner: UNT Libraries Government Documents Department
 Collection: Technical Report Archive and Image Library
Some experimental effects of afterbody shape on the zero-lift drag of bodies for Mach numbers between 0.8 and 1.3

Some experimental effects of afterbody shape on the zero-lift drag of bodies for Mach numbers between 0.8 and 1.3

Date: October 1, 1953
Creator: Stoney, William E , Jr
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Pressure measurements on a sharply converging fuselage afterbody with jet on and off at Mach numbers from 0.8 to 1.6

Pressure measurements on a sharply converging fuselage afterbody with jet on and off at Mach numbers from 0.8 to 1.6

Date: August 10, 1950
Creator: Stoney, William E , Jr & Katz, Ellis
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Heat-transfer and pressure measurements on flat-faced cylinders at a Mach number of 2

Heat-transfer and pressure measurements on flat-faced cylinders at a Mach number of 2

Date: July 1, 1958
Creator: Stoney, William E , Jr & Markley, J Thomas
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Some effects of body cross-sectional shape, including sunken-canopy design, on drag as shown by rocket-powered-model tests at Mach numbers from 0.8 to 1.5

Some effects of body cross-sectional shape, including sunken-canopy design, on drag as shown by rocket-powered-model tests at Mach numbers from 0.8 to 1.5

Date: July 1, 1952
Creator: Stoney, William E , Jr & Putland, Leonard W
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Heat transfer measured on a flat-face cylinder in free flight at Mach numbers up to 13.9

Heat transfer measured on a flat-face cylinder in free flight at Mach numbers up to 13.9

Date: June 17, 1957
Creator: Stoney, William E , Jr & Swanson, Andrew G
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Transonic drag measurements of eight body-nose shapes

Transonic drag measurements of eight body-nose shapes

Date: February 5, 1954
Creator: Stoney, William E JR
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Zero-lift drag of a series of bomb shapes at Mach numbers from 0.60 to 1.10

Zero-lift drag of a series of bomb shapes at Mach numbers from 0.60 to 1.10

Date: July 26, 1956
Creator: Stoney, William E, Jr & Royall, John F
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Transonic Zero-Lift Drag Tests of Four Equivalent-Body-of-Revolution Models Representing Variations of the Convair F-102 Airplane

Transonic Zero-Lift Drag Tests of Four Equivalent-Body-of-Revolution Models Representing Variations of the Convair F-102 Airplane

Date: October 17, 1955
Creator: Stoney, William E., Jr.
Description: Four 0.01643-scale equivalent-body-of-revolution models, designed to aid in the evaluation of the relative merits of various degrees of redesign of the existing (1955) Convair F-102 airplane, were launched from the helium gun at Wallops Island, Va., to determine their zero-lift drag at Mach numbers from 0.8 to 1.3. The data are presented with only sufficient analysis to validate their general subsonic level. Estimated values of the friction drag are presented at all Mach numbers to allow a comparison of the pressure drag values alone.
Contributing Partner: UNT Libraries Government Documents Department
The Analysis of Permissible Explosives

The Analysis of Permissible Explosives

Date: 1916
Creator: Storm, C. G.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
A flight investigation and analysis of the lateral-oscillation characteristics of an airplane

A flight investigation and analysis of the lateral-oscillation characteristics of an airplane

Date: June 3, 1948
Creator: Stough, Carl J & Kauffman, William M
Description: None
Contributing Partner: UNT Libraries Government Documents Department