Calculation of Wing Bending Moments and Tail Loads Resulting from the Jettison of Wing Tips During a Symmetrical Pull-Up (open access)

Calculation of Wing Bending Moments and Tail Loads Resulting from the Jettison of Wing Tips During a Symmetrical Pull-Up

"A preliminary analytical investigation was made to determine the feasibility of the basic idea of controlled failure points as safety valves for the primary airplane structure. The present analysis considers the possibilities of the breakable wing tip which, in failing as a weak link, would relieve the bending moments on the wing structure. The analysis was carried out by computing the time histories of the wing and stabilizer angle of attack in a 10g pull-up for an XF8F airplane with tips fixed and comparing the results with those for the same maneuver, that is, elevator motion but with tips jettisoned at 8g" (p. 1).
Date: December 11, 1947
Creator: Boshar, John
Object Type: Report
System: The UNT Digital Library
A comparison with flight data of vertical-tail loads in various maneuvers estimated from sideslip angles and rudder deflections (open access)

A comparison with flight data of vertical-tail loads in various maneuvers estimated from sideslip angles and rudder deflections

Report presenting a comparison of the vertical-tail loads determined from pressure-distribution measurements in flight in various maneuvers with the corresponding vertical-tail loads. Some of the maneuvers investigated included slow rolls, steady sideslips, fishtails, and rolling pull-outs.
Date: December 11, 1947
Creator: Turner, Howard L.
Object Type: Report
System: The UNT Digital Library
Physics Division. Quarterly Report, Period Covered September, October and November 1947 (open access)

Physics Division. Quarterly Report, Period Covered September, October and November 1947

None
Date: December 11, 1947
Creator: unknown
Object Type: Report
System: The UNT Digital Library
Preliminary Tests to Determine the Maximum Lift of Wings at Supersonic Speeds (open access)

Preliminary Tests to Determine the Maximum Lift of Wings at Supersonic Speeds

Report presenting the results of a test program in a supersonic tunnel to determine the maximum lift of wings operating at supersonic speeds. A variety of wing plan forms of several thickness distributions were tested at a range of Mach numbers, Reynolds numbers, and angles of attack. The lift results, drag results, and Schileren photographs are described.
Date: December 11, 1947
Creator: Gallagher, James J. & Mueller, James N.
Object Type: Report
System: The UNT Digital Library
Tests of Submerged Duct Installation on a Modified Airplane in the Ames 40- by 80-foot Wind Tunnel (open access)

Tests of Submerged Duct Installation on a Modified Airplane in the Ames 40- by 80-foot Wind Tunnel

Memorandum presenting an investigation of an NACA submerged intake installation on a modified fighter airplane conducted to determine the full-scale aerodynamic characteristics of this installation. Additionally, tests were conducted on the submerged inlet with revised entrance lips and deflectors to determine the configuration which would result in the best dynamic pressure recovery measured at the inlet for this installation without a major rework of the entrance.
Date: December 11, 1947
Creator: Martin, Norman J.
Object Type: Report
System: The UNT Digital Library
Texas Attorney General Opinion: V-451 (open access)

Texas Attorney General Opinion: V-451

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: Authority of State Board of Control to grant leaves for Course of Study to doctors and nurses of eleemosynary institutions without loss of salary.
Date: December 11, 1947
Creator: Texas. Attorney-General's Office.
Object Type: Text
System: The Portal to Texas History
Fraunhofer Diffraction Pattern Produced by a Slit of Varying Width and its Application to High Speed Cameras (open access)

Fraunhofer Diffraction Pattern Produced by a Slit of Varying Width and its Application to High Speed Cameras

Abstract: "A theoretical and experimental investigation is made of the diffraction pattern produced by a slit, whose aperture varies uniformly from a constant value A to zero. The results of this investigation are applied to a proposed high speed camera. It is shown that diffraction effects are very serious and cannot be neglected. It seems, unless the suggested design of this high speed camera is changed, the camera will be of little use for accurate measurements, and photographs will show too much blue to give details."
Date: November 11, 1947
Creator: Geiger, F. E. & Brixner, Berlyn
Object Type: Report
System: The UNT Digital Library
Report on Zirconium Nitride (open access)

Report on Zirconium Nitride

Report presenting the properties and method of preparation of zirconium nitride, a compound that was being considered for use in high temperatures due to its high melting point and hardness.
Date: November 11, 1947
Creator: Hall, George D.
Object Type: Report
System: The UNT Digital Library
Altitude-wind-tunnel investigation of thrust augmentation of a turbojet engine 3: performance with tail-pipe burning in standard-size tail pipe (open access)

Altitude-wind-tunnel investigation of thrust augmentation of a turbojet engine 3: performance with tail-pipe burning in standard-size tail pipe

From Introduction: "Evaluation of tail-pipe burning in this engine with a larger tail-pipe combustion chamber is discussed in reference 1. Results of investigations on tail-pipe burning in this engine at static sea-level conditions are presented in reference 2. An investigation of thrust augmentation by means of injecting water at the inlet of an axial-flow compressor engine is discussed in reference 3."
Date: August 11, 1947
Creator: Fleming, William A. & Golladay, Richard L.
Object Type: Report
System: The UNT Digital Library
THE EXTRACTION OF IONIUM BY ORGANIC SOLVENTS (open access)

THE EXTRACTION OF IONIUM BY ORGANIC SOLVENTS

None
Date: August 11, 1947
Creator: Hyde, E.K. & Tolmach, J.
Object Type: Report
System: The UNT Digital Library
Investigation of the I-40 Jet-Propulsion Engine in the Cleveland Altitude Wind Tunnel. V - Operational Characteristics, 5, Operational Characteristics (open access)

Investigation of the I-40 Jet-Propulsion Engine in the Cleveland Altitude Wind Tunnel. V - Operational Characteristics, 5, Operational Characteristics

An investigation has been conducted in the Cleveland altitude wind tunnel to determine the operational characteristics of the I-40 jet-propulsion engine over a range of pressure altitudes from 10,000 to 50,000 feet and ram-pressure ratios from 1.00 to 1.76. Engine operational data were obtained with the engine in the standard configuration and with various modifications of the fuel system, the electrical system, and the combustion chambers. The effects of altitude and airspeed on operating speed range, starting, windmilling, acceleration, speed regulation, cooling, and vibration of the standard and modified engines were determined, and damage to parts was noted.
Date: July 11, 1947
Creator: Golladay, Richard L. & Gendler, Stanley L.
Object Type: Report
System: The UNT Digital Library
Texas Attorney General Opinion: V-299 (open access)

Texas Attorney General Opinion: V-299

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: Exemption from ad valorem taxes of buildings and land belonging to Hale County Cooperative Hospital.
Date: July 11, 1947
Creator: Texas. Attorney-General's Office.
Object Type: Text
System: The Portal to Texas History
Texas Attorney General Opinion: V-300 (open access)

Texas Attorney General Opinion: V-300

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: Whether the Assured Home Ownership Plan of the Equitable Life Assurance Society of the United States violates Article 5053, V.C.S.
Date: July 11, 1947
Creator: Texas. Attorney-General's Office.
Object Type: Text
System: The Portal to Texas History
Texas Attorney General Opinion: V-301 (open access)

Texas Attorney General Opinion: V-301

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: Reconsideration of Opinions O-178 and O-7011, relative to use of courthouse space by abstract firms in light of subsequent court decisions and the submitted facts.
Date: July 11, 1947
Creator: Texas. Attorney-General's Office.
Object Type: Text
System: The Portal to Texas History
Texas Attorney General Opinion: V-302 (open access)

Texas Attorney General Opinion: V-302

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: Authority of tax collector to collect taxes delinquent for past ten years and then issue certificate showing taxes paid prior thereto, though not paid but subject to plea of ten year limitation as provided in Article 7298, V.C.S.
Date: July 11, 1947
Creator: Texas. Attorney-General's Office.
Object Type: Text
System: The Portal to Texas History
Application of Ascorbic Acid Method to Uranium in Salvage Solutions (open access)

Application of Ascorbic Acid Method to Uranium in Salvage Solutions

Abstract: The erroneously high values for uranium content of salvage solutions as determined by the ether extraction-ascorbic acid procedure have been demonstrated to be due to the presence of colored organic materials in these solutions. Evaporation of such solutions to fumes of HC104 before extraction has been shown to be completely successful in preventing such interference while pretreatment with activated carbon is sufficiently successful for application in Control laboratories. Complete procedures for application of either protreatment and results of such application to composite salvage solutions received over a six-month period are included.
Date: June 11, 1947
Creator: Rothenberger, C. D. & Grimes, W. R.
Object Type: Report
System: The UNT Digital Library
Results of Flight Test of an Automatically Stabilized Model C (Swept Back) Four-Wing Tiamat (open access)

Results of Flight Test of an Automatically Stabilized Model C (Swept Back) Four-Wing Tiamat

"The results of the first flight test of a swept-back four-wing version of Tiamat (MX-570 model C) which was launched at the NACA Pilotless Aircraft Research Station at W4110PB Island, Va. are presented. In general, the flight behavior was close to that predicted by calculations based an stability theory and oscillating table tests of the autopilot. The flight test thus indicates that the techniques employed to predict automatic stability are valid and practical from an operational viewpoint" (p. 1).
Date: June 11, 1947
Creator: Seacord, Charles L., Jr. & Teitelbaum, J. M.
Object Type: Report
System: The UNT Digital Library
Supersonic Wave Drag of Sweptback Tapered Wings at Zero Lift (open access)

Supersonic Wave Drag of Sweptback Tapered Wings at Zero Lift

An analysis has been made of airfoil data taken on several NACA 16-series propeller airfoils from tests of 5-inch-chord models in the Langley 24 inch high-speed tunnel and l2-inch-chord models in the Langley 8 foot high-speed tunnel, This analysis has shown that the combined effects of Reynolds number changes and variations in airfoil characteristics resulting from differences in models and tunnels are such that when 5 inch-chord and l2-inch-chord data are applied to full-scale propeller design at or near the design condition, differences of less than 1 percent in efficiency will be involved.
Date: June 11, 1947
Creator: Margolis, Kenneth
Object Type: Report
System: The UNT Digital Library
Texas Attorney General Opinion: V-243 (open access)

Texas Attorney General Opinion: V-243

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: Authority of County Commissioner to spend special fund in road district.
Date: June 11, 1947
Creator: Texas. Attorney-General's Office.
Object Type: Text
System: The Portal to Texas History
Texas Attorney General Opinion: V-244 (open access)

Texas Attorney General Opinion: V-244

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: Obligation of county to purchase right-of-way for a highway across lands once annexed and then purportedly relinquished by a home rule city.
Date: June 11, 1947
Creator: Texas. Attorney-General's Office.
Object Type: Text
System: The Portal to Texas History
Texas Attorney General Opinion: V-245 (open access)

Texas Attorney General Opinion: V-245

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: Fees of county clerks for issuing and recording abstracts of judgments.
Date: June 11, 1947
Creator: Texas. Attorney-General's Office.
Object Type: Text
System: The Portal to Texas History
Observations on an aileron-flutter instability encountered on a 45 degree swept-back wing in transonic and supersonic flight (open access)

Observations on an aileron-flutter instability encountered on a 45 degree swept-back wing in transonic and supersonic flight

Report presenting a flight test of a supersonic research pilotless aircraft in which large-amplitude aileron oscillations, most likely aileron compressibility flutter, were encountered in the transonic and supersonic speed ranges. Results regarding power-on flight and coasting flight are provided.
Date: April 11, 1947
Creator: Pitkin, Marvin; Gardner, William N. & Curfman, Howard J., Jr.
Object Type: Report
System: The UNT Digital Library
Tests of a Horizontal-Tail Model through the Transonic Speed Range by the NACA Wing-Flow Method (open access)

Tests of a Horizontal-Tail Model through the Transonic Speed Range by the NACA Wing-Flow Method

"A 1/12-scale model of a horizontal tail of a fighter airplane was tested through the transonic speeds in the high-speed flow over an airplane wing, the surface of which served as a reflection plane for the model. Measurements of lift, elevator-hinge moment, angle of attack, and elevator angle were made in the Mach number range from 0.75 to 1.04 for elevator deflections ranging from 10 degrees to minus 10 degrees, and for angles of attack of minus 1.2 degrees, 0.4 degrees, and 3.4 degrees. The equipment used to measure the hinge moments of the model proved to be unsatisfactory, and for this reason the hinge-moment data are considered to be only qualitative" (p. 1).
Date: April 11, 1947
Creator: Adams, Richard E. & Silsby, Norman S.
Object Type: Report
System: The UNT Digital Library
Texas Attorney General Opinion: V-139 (open access)

Texas Attorney General Opinion: V-139

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: Approval of School Bus Driver Bond by County School Board where School District is receiving State aid under Article V, Acts 1945, 49th Leg., R.S., Senate Bill 167.
Date: April 11, 1947
Creator: Texas. Attorney-General's Office.
Object Type: Text
System: The Portal to Texas History