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Texas Attorney General Opinion: MS-119
Letter opinion 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, John Ben Shepperd, regarding a legal question submitted for clarification; Interpretation of limitation on number of persons whose travel expenses may be paid for attending a meeting.
Date:
March 9, 1954
Creator:
Texas. Attorney-General's Office.
Object Type:
Text
System:
The Portal to Texas History
Low-Speed Chordwise Pressure Distributions Near the Midspan Station of the Slotted Flap and Aileron of a 1/4-Scale Model of the Bell X-1 Airplane With a 4-Percent-Thick, Aspect-Ratio-4, Unswept Wing
Report presenting an investigation to determine the low-speed chordwise pressure distributions near the midspan station of the slotted flap and aileron of a model of the Bell X-1 airplane with a wing of aspect ratio 4, taper ratio 0.5, 0 degree sweepback of the 40-percent-chord line, and a modified NACA 64A004 airfoil section. Results regarding section pressure distribution and section normal-force and pitching-moment coefficients are provided.
Date:
March 9, 1954
Creator:
Moseley, William C., Jr. & Taylor, Robert T.
Object Type:
Report
System:
The UNT Digital Library
Preliminary investigation of the 'freeze-casting' method for forming refractory powders
An investigation of a method of preparing intricately shaped objects such as turbo-supercharger blades from refractory powders. The method consists of preparing an extremely thick slip of materials like titanium carbide with a small amount of binder, casting the slip in a mold, and freezing to retain the shape of the casting. Results regarding the applicability of the method and factors affecting soundness, are provided.
Date:
March 9, 1954
Creator:
Maxwell, W. A.; Gurnick, R. S. & Francisco, A. C.
Object Type:
Report
System:
The UNT Digital Library
Flight Investigation of Engine Nacelles and Wing Vertical Position on the Drag of a Delta-Wing Airplane Configuration Form Mach Number 0.8 to 2.0
Report presenting flight testing of a 60 degree delta wing (NACA 65A003 airfoil section) mounted in midwing and high-wing positions on a modified transonic body from Mach numbers 0.8 to 2.0. The high-wing configuration without nacelles had higher drag coefficients than the midwing configuration without nacelles, but both configurations had approximately the same longitudinal distribution and frontal area. Results regarding nacelle internal drag, configuration drag, nacelle drag coefficient, and normal-force coefficient are provided.
Date:
March 9, 1954
Creator:
Judd, Joseph H.
Object Type:
Report
System:
The UNT Digital Library
The Effects of Horizontal-Tail Height and a Partial-Span Leading-Edge Extension on the Static Longitudinal Stability of a Wing-Fuselage-Tail Combination Having a Sweptback Wing
Memorandum presenting an investigation made to valuate the effects of vertical height of the horizontal tail on the static longitudinal stability of a model with a wing with 35 degrees of sweepback, an aspect ratio of 4.5, a taper ratio of 0.5, and NACA 64A010 sections. The investigation also included the effects of adding a partial-span, leading-edge chord extension to the outer portions of the wing. Results regarding the effect of tail height, wing-wake and local downwash measurements, and effect of a leading-edge extension are provided.
Date:
March 9, 1954
Creator:
Bandettini, Angelo & Selan, Ralph
Object Type:
Report
System:
The UNT Digital Library
The Effects of Circular End Plates on the Lift, Drag, and Pitching Moment at Subsonic and Supersonic Speeds on a Modified Triangular Wing Having an Aspect Ratio of 2, a Taper Ratio of 0.33, and a 45 Degree Swept Leading Edge
Memorandum presenting an investigation made of the effects of circular end plates on the aerodynamic characteristics of a modified triangular wing of aspect ratio 2 and taper ratio 0.33. The experimental results show that the addition of end plates produces so slight a difference in the total change in static longitudinal stability with Mach number in the range from 0.6 to 1.9 that no beneficial effects on the trim drag may be realized.
Date:
March 9, 1954
Creator:
Petersen, Robert B.
Object Type:
Report
System:
The UNT Digital Library
Monthly Progress Report No. 130
The following report is a general monthly progress report conducted by the radiation laboratory of the University of California discussing experimental physics, theoretical physics, the MTA target physics program, accelerator construction and operation, biology and medicine, and a plant and equipment report. The period being covered is January 15, 1954 to February 15, 1954.
Date:
March 9, 1954
Creator:
Lawrence Radiation Laboratory
Object Type:
Report
System:
The UNT Digital Library