Wind-Tunnel Investigation of Mutual Interference Loads on a Supersonic Bomber Configuration and Store During Separation at Mach Numbers of 1.57, 1.77, and 2.01 (open access)

Wind-Tunnel Investigation of Mutual Interference Loads on a Supersonic Bomber Configuration and Store During Separation at Mach Numbers of 1.57, 1.77, and 2.01

Report discussing an investigation into the mutual interference loads on a supersonic bomber configuration and store during separation of the store. Tests were performed at several airplane angles of attack, store angles of attack, and airplane sidestep angles. The aerodynamic characteristics of the various components and coefficients of forces are provided in tables.
Date: October 25, 1957
Creator: Morris, Owen G. & Turner, Kenneth L.
Object Type: Report
System: The UNT Digital Library
Wind-Tunnel Tests of a Series of Practice Bombs (open access)

Wind-Tunnel Tests of a Series of Practice Bombs

Report discussing zero-lift drag data for several bomb configurations at various Mach numbers. Seven configurations were tested with different combinations of interchangeable noses and tail cones with fins, some with different surface conditions. Surface conditions were not found to affect the drag, but the thickness of the tail fins and shape of the noses did change the shape of the drag curve.
Date: October 25, 1957
Creator: Ward, Donald H.
Object Type: Report
System: The UNT Digital Library
Design and experimental investigation of a single-stage turbine with a downstream stator (open access)

Design and experimental investigation of a single-stage turbine with a downstream stator

The high-work-output turbine had an experimental efficiency of 0.830 at the design point and a maximum efficiency of 0.857. The downstream stator was effective in providing axial flow out of the turbine for almost the whole range of turbine operation.
Date: January 25, 1957
Creator: Plohr, Henry W.; Holeski, Donald E. & Forrette, Robert E.
Object Type: Report
System: The UNT Digital Library
Pressure Measurements at Transonic and Low Supersonic Speeds on a Thin Conical Cambered Low-Aspect-Ratio Delta Wing in Combination With Basic and Indented Bodies (open access)

Pressure Measurements at Transonic and Low Supersonic Speeds on a Thin Conical Cambered Low-Aspect-Ratio Delta Wing in Combination With Basic and Indented Bodies

Report discussing pressure distributions on a thin conical cambered low-aspect-ratio delta wing over a range of Mach numbers. Combinations tested included the wing in combination with a basic Sears-Haack body and a body indented symmetrically for Mach number 1.2. Results regarding wing pressure distributions, effects of body indentation on the wing pressure, body pressure distributions, and effects of body indentation on body pressures are presented.
Date: September 25, 1957
Creator: Mugler, John P., Jr.
Object Type: Report
System: The UNT Digital Library
Compressibility Effects on a Hovering Helicopter Rotor Having an NACA 0018 Root Airfoil Tapering to an NACA 0012 Tip Airfoil (open access)

Compressibility Effects on a Hovering Helicopter Rotor Having an NACA 0018 Root Airfoil Tapering to an NACA 0012 Tip Airfoil

Report presenting an investigation to determine the effects of compressibility on the hovering performance and the blade pitching moments of a helicopter rotor with a tip airfoil, a root airfoil, and twist. Results regarding hovering performance, rotor-blade pitching moments, rotor profile-drag torque, and a comparison with two-dimensional drag-divergence data are provided.
Date: September 25, 1957
Creator: Powell, Robert D., Jr.
Object Type: Report
System: The UNT Digital Library
Investigation of the Low-Speed Stability and Control Characteristics of a 1/7-Scale Model of the North American X-15 Airplane (open access)

Investigation of the Low-Speed Stability and Control Characteristics of a 1/7-Scale Model of the North American X-15 Airplane

Report presenting an investigation of the low-speed power-on stability and control characteristics of a free-flying model of the North American X-15 airplane. Results regarding the longitudinal stability and control, lateral stability, and lateral control are provided. Longitudinal stability was low, but it was considered to be satisfactory up to an angle of attack of about 30 degrees.
Date: June 25, 1957
Creator: Boisseau, Peter C.
Object Type: Report
System: The UNT Digital Library
Free-Flight Investigation of the Drag of a Model of a 60 Degree Delta-Wing Bomber With Strut-Mounted Siamese Nacelles and Indented Fuselage at Mach Numbers From 0.80 to 1.35 (open access)

Free-Flight Investigation of the Drag of a Model of a 60 Degree Delta-Wing Bomber With Strut-Mounted Siamese Nacelles and Indented Fuselage at Mach Numbers From 0.80 to 1.35

Memorandum presenting a model of a 60 degree delta-wing bomber with strut-mounted Siamese nacelles, which was designed, with the use of a symmetrical fuselage indentation, to have a smooth average area distribution at a Mach number of 1.20. The results show that the configuration drag rise was significantly higher than that from the equivalent-body tests and area-rule theory throughout the Mach number range. Results regarding total drag and pressure drag are provided.
Date: September 25, 1957
Creator: Hoffman, Sherwood
Object Type: Report
System: The UNT Digital Library
Tolerable Limits of Oscillatory Accelerations Due to Rolling Motions Experienced by One Pilot During Automatic-Interceptor Flight Tests (open access)

Tolerable Limits of Oscillatory Accelerations Due to Rolling Motions Experienced by One Pilot During Automatic-Interceptor Flight Tests

Report presenting limited flight-test data obtained from an automatically controlled interceptor during runs in which oscillatory rolling motions occurred that were then compared to the pilot's comments about his ability to tolerate the imposed lateral oscillations. The alleviation of the undesirable effects of oscillatory lateral accelerations and their effects on piloting task were also considered. The marginally tolerable limit of acceleration forces on the pilot's head was found to be about 0.4 to 0.5g.
Date: January 25, 1957
Creator: Brissenden, Roy F.; Cheatham, Donald C. & Champine, Robert A.
Object Type: Report
System: The UNT Digital Library
Theoretical performance of liquid hydrogen and liquid fluorine as a rocket propellant for a chamber pressure of 600 pounds per square inch absolute (open access)

Theoretical performance of liquid hydrogen and liquid fluorine as a rocket propellant for a chamber pressure of 600 pounds per square inch absolute

Report presenting theoretical rocket performance for frozen and equilibrium composition during expansion for the propellant combination of liquid hydrogen and liquid fluorine at a chamber pressure of 600 pounds per square inch absolute and several pressure ratios and oxidant-fuel ratios. The parameters included were specific impulse, combustion-chamber temperature, nozzle-exit temperature, molecular weight, characteristic velocity, coefficient of thrust, ratio of nozzle-exit area to throat area, specific heat at constant pressure, isentropic exponent, viscosity, and thermal conductivity.
Date: January 25, 1957
Creator: Fortini, Anthony & Huff, Vearl N.
Object Type: Report
System: The UNT Digital Library
Aerodynamic Characteristics of Missile Configurations With Wings of Low Aspect Ratio for Various Combinations of Forebodies, Afterbodies, and Nose Shapes for Combined Angles of Attack and Sideslip at a Mach Number of 2.01 (open access)

Aerodynamic Characteristics of Missile Configurations With Wings of Low Aspect Ratio for Various Combinations of Forebodies, Afterbodies, and Nose Shapes for Combined Angles of Attack and Sideslip at a Mach Number of 2.01

"An investigation has been made in the Langley 4-by-4-foot supersonic pressure tunnel to determine the aerodynamic characteristics of a series of missile configurations having low-aspect-ratio wings at a Mach number of 2.01. The effects of wing plan form and size, length-diameter ratio, forebody and afterbody length, boattailed and flared afterbodies, and component force and moment data are presented for combined angles of attack and sideslip to about 28 degrees. No analysis of the data was made in this report" (p. 1).
Date: June 25, 1957
Creator: Robinson, Ross B.
Object Type: Report
System: The UNT Digital Library
Transonic Investigation of Effects of Spanwise and Chordwise External Store Location and Body Contouring on Aerodynamic Characteristics of 45 Degree Sweptback Wing-Body Configuration (open access)

Transonic Investigation of Effects of Spanwise and Chordwise External Store Location and Body Contouring on Aerodynamic Characteristics of 45 Degree Sweptback Wing-Body Configuration

Report presenting an investigation to determine the effects of spanwise and chordwise external store location on the aerodynamic characteristics of a cambered 45 degree sweptback wing-body configuration at a range of Mach numbers. Information about the drag characteristics of the various configurations, lift characteristics, and longitudinal stability characteristics is presented.
Date: September 25, 1957
Creator: Pearson, Albin O.
Object Type: Report
System: The UNT Digital Library
Comparison of low-lift drag at Mach numbers from 0.74 to 1.37 of rocket-boosted models having externally braced wings and cantilever wings (open access)

Comparison of low-lift drag at Mach numbers from 0.74 to 1.37 of rocket-boosted models having externally braced wings and cantilever wings

Report presenting an investigation to determine whether the low-lift drag of a rocket-model airplane-like configuration could be reduced at transonic and low supersonic Mach numbers by reducing wing thickness while external braces were used to provide the necessary bending strength. The investigation was conducted with two rocket models of aspect ratio 3.04, and unswept braced tapered wings mounted on fuselages with the same fineness ratios and cross-sectional area distributions. Data was compared to a previous study involving a model with a thicker cantilever wing.
Date: September 25, 1957
Creator: Dickens, Waldo L. & Hastings, Earl C., Jr.
Object Type: Report
System: The UNT Digital Library
Theoretical Investigation of the Attack Phase of an Automatic Interceptor System at Supersonic Speeds With Particular Attention to Aerodynamic and Dynamic Representation of the Interceptor (open access)

Theoretical Investigation of the Attack Phase of an Automatic Interceptor System at Supersonic Speeds With Particular Attention to Aerodynamic and Dynamic Representation of the Interceptor

Report presenting a theoretical investigation of the attack phase of an automatically controlled interceptor. Three types of control systems were simulated on an analog computer: a modern high-speed interceptor, a dynamically perfect radar-controlled director-type guidance system for a lead-collision course, and a velocity-type automatic pilot. The primary flight maneuver tested was a 5g climbing turn with roll and acceleration commands applied simultaneously.
Date: January 25, 1957
Creator: Sherman, Windsor L. & Schy, Albert A.
Object Type: Report
System: The UNT Digital Library
Texas Attorney General Opinion: WW-111 (open access)

Texas Attorney General Opinion: WW-111

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, Will Wilson, regarding a legal question submitted for clarification: Time allowed for the Governor to act on Bills presented to him after passage by the Legislature.
Date: April 25, 1957
Creator: Texas. Attorney-General's Office.
Object Type: Text
System: The Portal to Texas History
Texas Attorney General Opinion: WW-176 (open access)

Texas Attorney General Opinion: WW-176

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, Will Wilson, regarding a legal question submitted for clarification: Does the Retrieve State Farm, a unit of the Texas Prison System, have the authority to run a fence across Buffalo Camp Bayou at a point entirely within the prison owned property.
Date: July 25, 1957
Creator: Texas. Attorney-General's Office.
Object Type: Text
System: The Portal to Texas History
Texas Attorney General Opinion: WW-218 (open access)

Texas Attorney General Opinion: WW-218

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, Will Wilson, regarding a legal question submitted for clarification: Whether or not the Commissioners' Court of Calhoun County is subject to a requirement of a city ordinance for the payment of fees, charges or assessments for permits for the demolition of the old buildings and the construction of a new building.
Date: September 25, 1957
Creator: Texas. Attorney-General's Office.
Object Type: Text
System: The Portal to Texas History
Texas Attorney General Opinion: WW-8 (open access)

Texas Attorney General Opinion: WW-8

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, Will Wilson, regarding a legal question submitted for clarification: Liability of a volunteer fire department for payment of sales tax on motor vehicle to be used as a fire truck.
Date: January 25, 1957
Creator: Texas. Attorney-General's Office.
Object Type: Text
System: The Portal to Texas History
Texas Attorney General Opinion: WW-34 (open access)

Texas Attorney General Opinion: WW-34

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, Will Wilson, regarding a legal question submitted for clarification: Constitutionality of Senate Bill 103, of the 55th Legislature, prescriving the maximum working hours for Firemen, on a graduated basis in regard to the population of a County, and related questions.
Date: February 25, 1957
Creator: Texas. Attorney-General's Office.
Object Type: Text
System: The Portal to Texas History
Texas Attorney General Opinion: WW-38 (open access)

Texas Attorney General Opinion: WW-38

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, Will Wilson, regarding a legal question submitted for clarification; Deadline for filing application to appear on the official ballot at the Special Senatorial Election to be held April 2, 1957.
Date: February 25, 1957
Creator: Texas. Attorney-General's Office.
Object Type: Text
System: The Portal to Texas History
Texas Attorney General Opinion: WW-74 (open access)

Texas Attorney General Opinion: WW-74

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, Will Wilson, regarding a legal question submitted for clarification: Whether or not the royalty interest and fee interest conveyed in trust to the First National Bank of Longview for the use and benefit of the Roy H. Laird Memorial Hospital owned by the City of Kilgore would be exempt from taxation.
Date: March 25, 1957
Creator: Texas. Attorney-General's Office.
Object Type: Text
System: The Portal to Texas History
Texas Attorney General Opinion: WW-75 (open access)

Texas Attorney General Opinion: WW-75

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, Will Wilson, regarding a legal question submitted for clarification: Certification of candidates is a special election where his application was mailed on that last day for filing but was not received until the following day.
Date: March 25, 1957
Creator: Texas. Attorney-General's Office.
Object Type: Text
System: The Portal to Texas History
Texas Attorney General Opinion: WW-79 (open access)

Texas Attorney General Opinion: WW-79

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, Will Wilson, regarding a legal question submitted for clarification: Authority of the Commissioners' Court of a County to pay the salaries of a secretary and business manager for a Soil Conservation District.
Date: March 25, 1957
Creator: Texas. Attorney-General's Office.
Object Type: Text
System: The Portal to Texas History
Texas Attorney General Opinion: WW-262 (open access)

Texas Attorney General Opinion: WW-262

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, Will Wilson, regarding a legal question submitted for clarification: Whether deceased joint tenant's interest is subject to inheritance tax under submitted facts.
Date: September 25, 1957
Creator: Texas. Attorney-General's Office.
Object Type: Text
System: The Portal to Texas History
Texas Attorney General Opinion: WW-304 (open access)

Texas Attorney General Opinion: WW-304

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, Will Wilson, regarding a legal question submitted for clarification: The status of a member of a Board or Commission whose appointive term has expired during the recess of the Senate and whose successor has not been appointed and submitted to the Senate of the First Session of the Legislature convening after the expiration of the member's term.
Date: November 25, 1957
Creator: Texas. Attorney-General's Office.
Object Type: Text
System: The Portal to Texas History