Serial/Series Title

Investigation of Equilibrium Temperatures and Average Laminar Heat-Transfer Coefficients for the Front Half of Swept Circular Cylinders at a Mach Number of 6.9 (open access)

Investigation of Equilibrium Temperatures and Average Laminar Heat-Transfer Coefficients for the Front Half of Swept Circular Cylinders at a Mach Number of 6.9

Report presenting the average heat-transfer coefficients and equilibrium temperatures for the front half of an isothermal cylinder with a laminar boundary layer as determined by wind tunnel testing at Mach number 6.9 and a range of Reynolds numbers and sweep angles.
Date: August 18, 1955
Creator: Feller, William V.
System: The UNT Digital Library
Experimental investigation of a transonic compressor rotor with a 1.5-inch chord length and an aspect ratio of 3.0 2: blade-element performance (open access)

Experimental investigation of a transonic compressor rotor with a 1.5-inch chord length and an aspect ratio of 3.0 2: blade-element performance

Report presenting a transonic compressor rotor with double-circular-arc blade sections, which were designed and tested to investigate the aerodynamic effects of using a short blade chord and a high aspect ratio. The report presents the blade-element performance and performance analysis.
Date: August 18, 1955
Creator: Schwenk, Francis C. & Tysl, Edward R.
System: The UNT Digital Library
A preliminary investigation of static-pressure changes associated with combustion of aluminum borohydride in a supersonic wind tunnel (open access)

A preliminary investigation of static-pressure changes associated with combustion of aluminum borohydride in a supersonic wind tunnel

Report presenting static-pressure changes resulting from steady combustion of aluminum borohydride in a supersonic wind tunnel. Static pressures were measured along the top wall of a tunnel adjacent to the flame that filled the upper portion of the test section. Results regarding the static-pressure increases, effect of change in fuel-injection rate, and effect of tunnel boundary layer on the character of the heat-addition region are provided.
Date: August 18, 1955
Creator: Dorsch, Robert G.; Serafini, John S. & Fletcher, Edward A.
System: The UNT Digital Library
Investigation of the Effects of Bomb-Bay Configuration Upon the Aerodynamic Characteristics of a Body With Circular Cross Section at Supersonic Speeds (open access)

Investigation of the Effects of Bomb-Bay Configuration Upon the Aerodynamic Characteristics of a Body With Circular Cross Section at Supersonic Speeds

Memorandum presenting an investigation in the 9-inch supersonic tunnel to ascertain the lift, drag, and pitching moment associated with typical body-bomb-bay combinations with and without the bomb. Measurements were made at a range of angles of attack, Mach numbers, and Reynolds numbers.
Date: August 18, 1955
Creator: Rainey, Robert W.
System: The UNT Digital Library
Some Dielectric Properties of Suspensions of Boron Powders in Mineral Oil (open access)

Some Dielectric Properties of Suspensions of Boron Powders in Mineral Oil

Memorandum presenting measurements of the dielectric constant for suspensions of two types of boron powder in mineral oil as a function of concentration of boron particles, moisture content, temperature, and frequency of oscillation. Also investigated were the effects of boron-powder concentration and moisture content on the dielectric losses of mineral-oil suspensions of the two boron powders.
Date: August 18, 1955
Creator: Altshuller, Aubrey P.
System: The UNT Digital Library