Altitude performance of annular combustor type turbojet engine with JFC-2 fuel (open access)

Altitude performance of annular combustor type turbojet engine with JFC-2 fuel

An investigation was made comparing the performance of JFC-2 fuel and unleaded, clear gasoline in a 3000-pound-thrust turbojet engine. The JFC-2 fuel was a blend of percent diesel fuel and 25 percent aviation gasoline. Engine combustion efficiency was equal to that obtained with gasoline at rated engine speed and altitudes up to 35,000 feet, but at lower engine speeds or at higher altitudes the JFC-2 fuel gave lower combustion efficiency. No discernible difference was obtained in starting or low-speed combustiion blow-out characteristics of the two fuels. Turbine-discharge radial temperature profiles were nearly the same at altitudes up to 35,000 feet.
Date: February 5, 1952
Creator: Useller, James W.; Harp, James L., Jr. & Barson, Zelmar
Object Type: Report
System: The UNT Digital Library
Loitering and range performance of turbojet-powered aircraft determined by off-design engine cycle analysis (open access)

Loitering and range performance of turbojet-powered aircraft determined by off-design engine cycle analysis

From Summary: "The loitering and range performance of airplanes equipped with several different turbojet engines was analytically investigated by applying the results of off-design cycle analyses to specific airplane characteristics. The method of off-design cycle analysis is presented herein and is verified by a check with experimental data. For all engines considered, the loitering and the range fuel flows obtained with rated tail-pipe nozzle area, variable engine speed operations were within 2 or 3 percent of the optimum fuel flow obtainable with any method of engines operation. The optimum loitering altitude generally occurred between approximately 25,000 and 35,000 feet with corresponding optimum flight Mach numbers of 0.4 to 0.65. In general, the optimum range fuel flows occurred at 3000 to 5000 feet higher altitude and at approximately 0.15 higher flight Mach numbers than the optimum loitering fuel flow."
Date: February 5, 1952
Creator: Koutz, Stanley L. & Hensley, Reece V.
Object Type: Report
System: The UNT Digital Library
Texas Attorney General Opinion: V-1401 (open access)

Texas Attorney General Opinion: V-1401

Document issued by the Office of the Attorney General of Texas in Austin, Texas, providing an interpretation of Texas law. It provides the opinion of the Texas Attorney General, Price Daniel, regarding a legal question submitted for clarification: Legality of the County Clerk recording the plat of a subdivision within five miles of an incorporated city when it has been approved by the City Planning Commission but not by the Commissioners' Court.
Date: February 5, 1952
Creator: Texas. Attorney-General's Office.
Object Type: Text
System: The Portal to Texas History
Texas Attorney General Opinion: V-1402 (open access)

Texas Attorney General Opinion: V-1402

Document issued by the Office of the Attorney General of Texas in Austin, Texas, providing an interpretation of Texas law. It provides the opinion of the Texas Attorney General, Price Daniel, regarding a legal question submitted for clarification: Statutory penalty for failure of a railroad to keep its ticket office open for half an hour prior to the departure of trains which are late.
Date: February 5, 1952
Creator: Texas. Attorney-General's Office.
Object Type: Text
System: The Portal to Texas History