Investigation of altitude ignition, acceleration and steady-state operation with single combustor of J47 turbojet engine (open access)

Investigation of altitude ignition, acceleration and steady-state operation with single combustor of J47 turbojet engine

Report describing an investigation conducted with a single combustor from a J47 turbojet engine using weathered aviation gasoline and several spark-plug modifications to determine altitude ignition, acceleration, and steady-state operating characteristics. Results regarding ignition, acceleration, altitude operational limits, combustion efficiency, and pressure loss are provided.
Date: March 5, 1951
Creator: Cook, William P. & Butze, Helmut F.
System: The UNT Digital Library
Investigation of the effects of geometric changes in an underwing pylon suspended external store installation on the aerodynamic characteristics of a 45 degree sweptback wing at high subsonic speeds (open access)

Investigation of the effects of geometric changes in an underwing pylon suspended external store installation on the aerodynamic characteristics of a 45 degree sweptback wing at high subsonic speeds

Report presenting an investigation in the high-speed 7- by 10-foot tunnel through a range of Mach numbers to determine the effects of external-store fineness ratio, store shape, store chordwise position, pylon thickness, pylon length, and pylon sweep angle on the aerodynamic characteristics of a number of underwing pylon-suspended external stores in combination with a 45 degree sweptback semispan wing and fuselage.
Date: March 5, 1951
Creator: Spreemann, Kenneth P. & Alford, William J., Jr.
System: The UNT Digital Library
Experimental investigation of tail-pipe-burner design variables (open access)

Experimental investigation of tail-pipe-burner design variables

Report summarizing several experimental tail-pipe-burner investigations to indicate the effects of tail-pipe-burner design variables on the performance and operating characteristics. Most of the configurations were investigated over a wide range of altitudes and flight Mach numbers. The results indicate the desirable design features of a tail-pipe burner that will operate with high combustion efficiency and exhaust-gas temperature up to an altitude of approximately 50,000 feet.
Date: March 5, 1951
Creator: Fleming, W. A.; Conrad, E. William & Young, W. A.
System: The UNT Digital Library
Characteristics of flow over inclined bodies of revolution (open access)

Characteristics of flow over inclined bodies of revolution

From Summary: "Experimental force, moment, and center-of-pressure variations for a large number of bodies of revolution have been compared with the calculated characteristics based on the approximate theory developed in NACA-RM-A9I26. The bodies varied in fineness ratio from 4.5 to 21.1, from blunt unboattailed bodies to airship hulls, and the experimental results are given for widely varying Mach number ranges of angle of attack. It is shown that the lift and drag characteristics are fairly accurately predicted by the theory but that the actual center of pressure is more rearward than the theory indicates."
Date: March 5, 1951
Creator: Allen, H. Julian & Perkins, Edward W.
System: The UNT Digital Library
Progress Report on the Argonne-Oak Ridge Digital Computer (open access)

Progress Report on the Argonne-Oak Ridge Digital Computer

Report issued by the Argonne National Laboratory discussing a progress report on the Argonne-Oak Ridge digital computer. This report is an interim report, whose primary value is that it has forced those engaged in the work to give concrete expression to what they have been doing and thinking about up to this point. This report includes tables, illustrations, and photographs.
Date: March 5, 1951
Creator: Birge, W. A.; Burdette, E. W.; Burks, A. W.; Chu, J. C.; Flanders, D. A.; Jacobsohn, D. H. et al.
System: The UNT Digital Library