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9
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8
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7
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7
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Collection
Texas Digital Newspaper Program
189
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130
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89
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86
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68
KXAS-NBC 5 News Collection
62
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35
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27
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26
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Results:
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605
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Pioneer Service Station
Exterior shot of Pioneer Service Station, 1100 Red River
Date:
May 31, 1956
Creator:
Douglass, Neal
Object Type:
Photograph
System:
The Portal to Texas History
Pioneer Service Station
Exterior shot of service station with car at pump, 1100 Red River
Date:
May 31, 1956
Creator:
Douglass, Neal
Object Type:
Photograph
System:
The Portal to Texas History
The Tulia Herald (Tulia, Tex), Vol. 47, No. 22, Ed. 1, Thursday, May 31, 1956
Weekly newspaper from Tulia, Texas that includes local, state and national news along with extensive advertising.
Date:
May 31, 1956
Creator:
Baggarly, H. M.
Object Type:
Newspaper
System:
The Portal to Texas History
The Bartlett Tribune and News (Bartlett, Tex.), Vol. 69, No. 44, Ed. 1, Friday, August 31, 1956
Weekly newspaper from Bartlett, Texas that includes local, state and national news along with extensive advertising.
Date:
August 31, 1956
Creator:
Ford, Robert C. & Ford, Nora Mae
Object Type:
Newspaper
System:
The Portal to Texas History
Breckenridge American (Breckenridge, Tex.), Vol. 36, No. 214, Ed. 1 Wednesday, October 31, 1956
Daily newspaper (except Sunday) from Breckenridge, Texas that includes local, state and national news along with extensive advertising.
Date:
October 31, 1956
Creator:
unknown
Object Type:
Newspaper
System:
The Portal to Texas History
Breckenridge American (Breckenridge, Tex.), Vol. 36, No. 107, Ed. 1 Thursday, May 31, 1956
Daily newspaper (except Sunday) from Breckenridge, Texas that includes local, state and national news along with extensive advertising.
Date:
May 31, 1956
Creator:
unknown
Object Type:
Newspaper
System:
The Portal to Texas History
Breckenridge American (Breckenridge, Tex.), Vol. 36, No. 149, Ed. 1 Tuesday, July 31, 1956
Daily newspaper (except Sunday) from Breckenridge, Texas that includes local, state and national news along with extensive advertising.
Date:
July 31, 1956
Creator:
unknown
Object Type:
Newspaper
System:
The Portal to Texas History
Breckenridge American (Breckenridge, Tex.), Vol. 36, No. 171, Ed. 1 Friday, August 31, 1956
Daily newspaper (except Sunday) from Breckenridge, Texas that includes local, state and national news along with extensive advertising.
Date:
August 31, 1956
Creator:
unknown
Object Type:
Newspaper
System:
The Portal to Texas History
Breckenridge American (Breckenridge, Tex.), Vol. 36, No. 22, Ed. 1 Tuesday, January 31, 1956
Daily newspaper (except Sunday) from Breckenridge, Texas that includes local, state and national news along with extensive advertising.
Date:
January 31, 1956
Creator:
unknown
Object Type:
Newspaper
System:
The Portal to Texas History
The Aspermont Star (Aspermont, Tex.), Vol. 59, No. 38, Ed. 1 Thursday, May 31, 1956
Weekly newspaper from Aspermont, Texas that includes local, state and national news along with extensive advertising.
Date:
May 31, 1956
Creator:
Welch, Lowell C.
Object Type:
Newspaper
System:
The Portal to Texas History
The Rusk Cherokeean. (Rusk, Tex.), Vol. 108, No. 49, Ed. 1 Thursday, May 31, 1956
Weekly newspaper from Rusk, Texas that includes local, state and national news along with extensive advertising.
Date:
May 31, 1956
Creator:
Whitehead, E. H.
Object Type:
Newspaper
System:
The Portal to Texas History
The Canadian Record (Canadian, Tex.), Vol. 67, No. 22, Ed. 1 Thursday, May 31, 1956
Weekly newspaper from Canadian, Texas that includes local, state and national news along with extensive advertising.
Date:
May 31, 1956
Creator:
Ezzell, Ben
Object Type:
Newspaper
System:
The Portal to Texas History
Lift, Drag, Static Stability, and Buffet Boundaries of a Model of the McDonnell F3H-1N Airplane at Mach Numbers from 0.40 to 1.27, TED No. NACA DE 351
"The National Advisory Committee for Aeronautics has conducted a flight test of a model approximating the McDonnell F3H-1N airplane configuration to determine its pitch-up and buffet boundaries, as well as the usual longitudinal stability derivatives obtainable from the pulsed- tail technique. The test was conducted by the freely flying rocket-boosted model technique developed at the Langley Laboratory; results were obtained at Mach numbers from 0.40 to 1.27 at corresponding Reynolds numbers of 2.6 x 10(exp 6) and 9.0 x 10(exp 6). The phenomena of pitch-up, buffet, and maximum lift were encountered at Mach numbers between 0.42 and 0.85" (p. 1).
Date:
January 31, 1956
Creator:
Crabill, Norman L.
Object Type:
Report
System:
The UNT Digital Library
Factors That Affect Operational Reliability of Turbojet Engines
The problem of improving operational reliability of turbojet engines is studied in a series of papers. Failure statistics for this engine are presented, the theory and experimental evidence on how engine failures occur are described, and the methods available for avoiding failure in operation are discussed. The individual papers of the series are Objectives, Failure Statistics, Foreign-Object Damage, Compressor Blades, Combustor Assembly, Nozzle Diaphrams, Turbine Buckets, Turbine Disks, Rolling Contact Bearings, Engine Fuel Controls, and Summary Discussion.
Date:
January 31, 1956
Creator:
Lewis Laboratory Staff
Object Type:
Report
System:
The UNT Digital Library
An experimental investigation at Mach numbers from 2.1 to 3.0 of circular-internal-contraction inlets with translating centerbodies
Report presenting the total-pressure recovery characteristics of three circular internal-compression inlets with translating centerbodies at a range of free-stream Mach numbers. The inlets differed only in the shape of the internal compression contours. Results regarding the maximum pressure recoveries and pressure-recovery characteristics are provided.
Date:
October 31, 1956
Creator:
Mossman, Emmett A. & Pfyl, Frank A.
Object Type:
Report
System:
The UNT Digital Library
A summary of NACA research on the strength and creep of aircraft structures at elevated temperatures
Report summarizing research on the strength and creep of aircraft structural elements and components at elevated temperatures. Experimental data for aluminum alloy columns, plates, stiffened panels, and multiweb box beams are presented for temperatures up to 600 degrees Fahrenheit and compared with results predicted from materials data.
Date:
May 31, 1956
Creator:
Heldenfels, Richard R. & Mathauser, Eldon E.
Object Type:
Report
System:
The UNT Digital Library
Static stability characteristics of a cambered-delta-wing model at high subsonic speeds
Report presenting an investigation at high subsonic speeds to determine the static stability characteristics of a cambered-delta-wing model with wing dihedral angles of 20 degrees and 50 degrees. Results regarding the longitudinal characteristics and lateral characteristics are provided.
Date:
October 31, 1956
Creator:
Moseley, William C., Jr.
Object Type:
Report
System:
The UNT Digital Library
Preflight and flight-test investigation of a 50-percent-magnesium 50-percent JP-4 slurry fuel in a twin engine ram-jet vehicle
Report presenting an investigation conducted by means of preflight and flight tests to determine the performance of a 50-percent-magnesium 50-percent JP-4 slurry fuel in a twin-engine ramjet test vehicle. Data were obtained over a range of Mach numbers. Although a successful flight test was carried out, the performance obtained from preflight testing was below theoretical values.
Date:
May 31, 1956
Creator:
Trout, Otto F., Jr. & Kennedy, Thomas L.
Object Type:
Report
System:
The UNT Digital Library
Heat Transfer on the Lifting Surfaces of a 60 Degree Delta Wing at Angle of Attack for Mach Number 1.98
Report presenting the heat transfer and pressures on the lifting surfaces of a 60 degree delta wing with NACA 65A005 profile at angles of attack up to 9 degrees. Results obtained are compared to values obtained from flat-plate theory.
Date:
May 31, 1956
Creator:
Carter, Howard S.
Object Type:
Report
System:
The UNT Digital Library
Wind-Tunnel Investigation of Two Vertical-Takeoff-and-Landing Jet Bomber Airplane Configurations at Mach Numbers of 1.94 and 2.40
Report presenting an investigation to obtain information about the basic aerodynamic characteristics of two vertical-take-off-and-landing jet bomber airplanes, one with a high wing and one with a low wing. Results regarding pitch and sideslip are provided. The high-tail configurations were found to have higher lift-drag ratios for both high- and low-wing models.
Date:
October 31, 1956
Creator:
Jones, Robert A. & Rainey, Robert W.
Object Type:
Report
System:
The UNT Digital Library
Flight Determination of the Lateral Handling Qualities of the Bell X-5 Research Airplane at 58.7 Degrees Sweepback
Memorandum presenting the Bell X-5 variable-sweep research airplane tested primarily at 58.7 degrees sweepback to determine the characteristics at transonic speeds of a fighter-type airplane with extreme sweepback. Some of the dynamic and static lateral stability characteristics have been discussed previously. Results regarding the lateral control, roll coupling, lateral problems at high lift, wing dropping, rudder oscillation at supersonic Mach numbers, and some pilots' impressions are also provided.
Date:
May 31, 1956
Creator:
Finch, Thomas W. & Walker, Joseph A.
Object Type:
Report
System:
The UNT Digital Library
Effect of Increase in Angle of Dead Rise on the Hydrodynamic Qualities of a Seaplane Configuration Incorporating High Wing Loading
Memorandum presenting an investigation to determine the effects of increase in angle of dead rise on the overall hydrodynamic characteristics of a seaplane having a length-beam ratio of 15 and a wing loading of 120 pounds per square foot. In general, increasing the angle of dead rise from 20 to 40 degrees and 60 degrees improved the trim limits of stability and the range of center-of-gravity positions for satisfactory take-off characteristics.
Date:
October 31, 1956
Creator:
Kapryan, Walter J. & Weinstein, Irving
Object Type:
Report
System:
The UNT Digital Library
Combined Effects of Wing Taper and Low Horizontal-Tail Position on Longitudinal Stability of a 45 Degree Sweptback Wing-Body Combination at Transonic Speeds
Report presenting an investigation of the combined effects of wing taper ratio and low horizontal-tail position on the static longitudinal stability of a 45 degree sweptback wing-body combination with an aspect ratio of 4 at a range of Mach numbers. Results regarding tail-off pitch characteristics, tail-on pitch characteristics, and effective flow characteristics over horizontal tail are provided.
Date:
October 31, 1956
Creator:
Spooner, Stanley H.
Object Type:
Report
System:
The UNT Digital Library
The Alto Herald (Alto, Tex.), No. 51, Ed. 1 Thursday, May 31, 1956
Weekly newspaper from Alto, Texas that includes local, state and national news along with extensive advertising.
Date:
May 31, 1956
Creator:
F. L. Weimar & Son
Object Type:
Newspaper
System:
The Portal to Texas History