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  Partner: UNT Libraries Government Documents Department
 Decade: 1950-1959
 Year: 1957
 Month: June
 Collection: Technical Report Archive and Image 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

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

Date: June 25, 1957
Creator: Robinson, Ross B
Description: 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.
Contributing Partner: UNT Libraries Government Documents Department
Aerodynamic Heating and Boundary-layer Transition on a 1/10-power nose shape in free flight at Mach numbers up to 6.7 and Free-stream Reynolds numbers up tp 16 x 10(exp 6)

Aerodynamic Heating and Boundary-layer Transition on a 1/10-power nose shape in free flight at Mach numbers up to 6.7 and Free-stream Reynolds numbers up tp 16 x 10(exp 6)

Date: June 17, 1957
Creator: Garland, Benjamine J; Swanson, Andrew G & Speegle, Katherine C
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Aerodynamics of Oscillating Control Surfaces at Transonic Speeds

Aerodynamics of Oscillating Control Surfaces at Transonic Speeds

Date: June 17, 1957
Creator: Clevenson, S. A. & Thompson, R. F.
Description: Aerodynamic forces and moments of oscillating control surfaces at transonic speeds.
Contributing Partner: UNT Libraries Government Documents Department
Airborne Radiometric Reconnaissance in the Wind River Basin, Wyoming

Airborne Radiometric Reconnaissance in the Wind River Basin, Wyoming

Date: June 1957
Creator: Loomis, Tom H. W. & Blair, Robert G.
Description: Abstract: A program of airborne radiometric reconnaissance for uranium was conducted in eastern Fremont and western Natrona Counties, in central Wyoming, during the summer and fall of 1954, by the U.S. Atomic Energy Commission.
Contributing Partner: UNT Libraries Government Documents Department
Altitude starting tests of a small solid propellant rocket

Altitude starting tests of a small solid propellant rocket

Date: June 21, 1957
Creator: Krawczoner, E. M. & Sloop, J. L.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Analyses for turbojet thrust augmentation with fuel-rich afterburning of hydrogen, diborane, and hydrazine

Analyses for turbojet thrust augmentation with fuel-rich afterburning of hydrogen, diborane, and hydrazine

Date: June 18, 1957
Creator: Morris, James F
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Analyses for turbojet thrust augmentation with fuel-rich afterburning of hydrogen, diborane, and hydrazine

Analyses for turbojet thrust augmentation with fuel-rich afterburning of hydrogen, diborane, and hydrazine

Date: June 18, 1957
Creator: Morris, J. F.
Description: Turbojet thrust augmentation with fuel-rich afterburning of hydrogen, diborane, and hydrazine.
Contributing Partner: UNT Libraries Government Documents Department
Analysis of Meteorological Tower Data, April 1950 - March 1952, Brookhaven National Laboratory

Analysis of Meteorological Tower Data, April 1950 - March 1952, Brookhaven National Laboratory

Date: June 1957
Creator: Singer, Irving A. & Raynor, Gilbert S.
Description: Report issued by the Brookhaven National Laboratory discussing data collected from two BNL meteorological towers. As stated in the introduction, "results are presented in graphic form rather than tabular form" (p. 1). This report includes tables, maps, illustrations, and photographs.
Contributing Partner: UNT Libraries Government Documents Department
Analysis of two-spool turboprop-engine characteristics

Analysis of two-spool turboprop-engine characteristics

Date: June 3, 1957
Creator: Davison, Elmer H
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Analytical investigation of fuel-cooled turbine blades with return-flow type of finned coolant passages

Analytical investigation of fuel-cooled turbine blades with return-flow type of finned coolant passages

Date: June 26, 1957
Creator: Nachtigall, Alfred J & Slone, Henry O
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Analytical Investigation of Fuel-cooled Turbine Blades With Return-flow Type of Finned Coolant Passages

Analytical Investigation of Fuel-cooled Turbine Blades With Return-flow Type of Finned Coolant Passages

Date: June 26, 1957
Creator: Nachtigall, A. J. & Slone, H. O.
Description: Fuel-cooled turbine blades with return-flow type of finned coolant passages.
Contributing Partner: UNT Libraries Government Documents Department
Analytical study of the comparative pitch-up behavior of several airplanes and correlation with pilot opinion

Analytical study of the comparative pitch-up behavior of several airplanes and correlation with pilot opinion

Date: June 12, 1957
Creator: Sadoff, Melvin; Stewart, John D & Cooper, George E
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Cascade investigation of cooling characteristics of a cast-finned air-cooled turbine blade for use in a turboprop engine

Cascade investigation of cooling characteristics of a cast-finned air-cooled turbine blade for use in a turboprop engine

Date: June 12, 1957
Creator: Stepka, Francis S; Richards, Hadley T & Hickel, Robert O
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Cascade Investigation of Cooling Characteristics of a Castfinned Air-cooled Turbine Blade for Use in a Turboprop Engine

Cascade Investigation of Cooling Characteristics of a Castfinned Air-cooled Turbine Blade for Use in a Turboprop Engine

Date: June 12, 1957
Creator: Hickel, R. O.; Richards, H. T. & Stepka, F. S.
Description: Cascade investigation of cooling characteristics of air-cooled turbine blade for use in turboprop engine.
Contributing Partner: UNT Libraries Government Documents Department
Charts for estimating the effects of short-period stability characteristics on airplane vertical-acceleration and pitch-angle response in continuous atmospheric turbulence

Charts for estimating the effects of short-period stability characteristics on airplane vertical-acceleration and pitch-angle response in continuous atmospheric turbulence

Date: June 1, 1957
Creator: Pratt, Kermit G & Bennett, Floyd V
Description: None
Contributing Partner: UNT Libraries Government Documents Department
The combinations of thermal and load stresses for the onset of permanent buckling in plates

The combinations of thermal and load stresses for the onset of permanent buckling in plates

Date: June 1, 1957
Creator: Zender, George W & Pride, Richard A
Description: A simple and practical method for evaluating the onset of permanent buckling in plates in the presence of combined thermal and compressive load stresses is outlined. A particular application of the method shows reasonable agreement with tests of 17-7 PH stainless-steel square tubes. The results indicate that the compressive load stress which the plate can support at the onset of permanent buckling is substantially reduced as the temperature difference of the plate and adjoining members increases.
Contributing Partner: UNT Libraries Government Documents Department
A comparison of carrier approach speeds as determined from flight tests and from pilot-operated simulator studies

A comparison of carrier approach speeds as determined from flight tests and from pilot-operated simulator studies

Date: June 19, 1957
Creator: Drinkwater, Fred J , III & White, Maurice D
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Compressible laminar boundary layer over a yawed infinite cylinder with heat transfer and arbitrary Prandtl number

Compressible laminar boundary layer over a yawed infinite cylinder with heat transfer and arbitrary Prandtl number

Date: June 1, 1957
Creator: Reshotko, Eli & Beckwith, Ivan E.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Design and engine evaluation of a semistrut corrugated air-cooled turbine blade for operation at a tip speed of 1300 feet per second

Design and engine evaluation of a semistrut corrugated air-cooled turbine blade for operation at a tip speed of 1300 feet per second

Date: June 26, 1957
Creator: Meyer, Andre' J , Jr; Kemp, Richard H & Morgan, William C
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Design and experimental evaluation of a light-weight turbine-wheel assembly

Design and experimental evaluation of a light-weight turbine-wheel assembly

Date: June 1, 1957
Creator: Morgan, W C & Kemp, R H
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Effect of fuel properties on liner temperatures in a single tubular turbojet combustor

Effect of fuel properties on liner temperatures in a single tubular turbojet combustor

Date: June 3, 1957
Creator: Butze, Helmut F
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Effect of hinge-line position on the oscillating hinge moments and flutter characteristics of a flap-type control at transonic speeds

Effect of hinge-line position on the oscillating hinge moments and flutter characteristics of a flap-type control at transonic speeds

Date: June 10, 1957
Creator: Thompson, Robert F & Moseley William C , JR
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Effect of Hinge-line Position on the Oscillating Hinge Moments and Flutter Characteristics of a Flap-type Control at Transonic Speeds

Effect of Hinge-line Position on the Oscillating Hinge Moments and Flutter Characteristics of a Flap-type Control at Transonic Speeds

Date: June 10, 1957
Creator: Moseley, W. C., Jr. & Thompson, R. F.
Description: Free oscillation test to determine hinge moment of trailing-edge, flap control surface with various hinge-line positions at transonic speed.
Contributing Partner: UNT Libraries Government Documents Department
Effect of transient heating on vibration frequencies of some simple wing structures

Effect of transient heating on vibration frequencies of some simple wing structures

Date: June 1, 1957
Creator: Vosteen, Louis F; Mcwithey, Robert R & Thomson, Robert G
Description: Thermal stresses, which may result from transient heating, can cause changes in the effective stiffness of wing structures. Some effects of this change in stiffness were investigated experimentally by radiantly heating three types of simple wing structures: a uniform plate, a solid double-wedge section, and a circular-arc multiweb-wing section. Changes in stiffness were determined by measuring the changes in natural frequency of vibration during transient heating. Some comparisons are made between theoretical calculations and the measured data.
Contributing Partner: UNT Libraries Government Documents Department
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