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  Partner: UNT Libraries Government Documents Department
 Decade: 1950-1959
 Year: 1957
 Month: August
 Collection: Technical Report Archive and Image Library
Aerodynamic Forces on a Vibrating Unstaggered Cascade

Aerodynamic Forces on a Vibrating Unstaggered Cascade

Date: August 1957
Creator: Soehngen, H.
Description: The unsteady aerodynamic forces, [based on two-dimensional incompressible flow considerations], are determined for an unstaggered cascade, the blades of which are vibrating in phase in an approach flow parallel to the blades.
Contributing Partner: UNT Libraries Government Documents Department
Aerodynamic heating of a thin, unswept, untapered, multiweb, aluminum-alloy wing at Mach numbers up to 2.67 as determined from a free-flight investigation of a rocket-propelled model

Aerodynamic heating of a thin, unswept, untapered, multiweb, aluminum-alloy wing at Mach numbers up to 2.67 as determined from a free-flight investigation of a rocket-propelled model

Date: August 6, 1957
Creator: Strass, H Kurt & Stephens, Emily W
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Aging Characteristics of Hastelloy B

Aging Characteristics of Hastelloy B

Date: August 12, 1957
Creator: Clausing, Robert E.; Patriarca, P. & Manly, W. D.
Description: Report issued by the Oak Ridge National Laboratory discussing the aging characteristics of the alloy Hastelloy B. Materials, equipment, experimental procedures, and results used to determine the characteristics of the alloy are presented. This report includes tables, illustrations, and photographs.
Contributing Partner: UNT Libraries Government Documents Department
Airplane measurements of atmospheric turbulence for altitudes between 20,000 and 55,000 feet over the western part of the United States

Airplane measurements of atmospheric turbulence for altitudes between 20,000 and 55,000 feet over the western part of the United States

Date: August 23, 1957
Creator: Coleman, Thomas L & Coe, Emilie C
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Altitude chamber evaluation of an aircraft liquid hydrogen fuel system used with a turbojet engine

Altitude chamber evaluation of an aircraft liquid hydrogen fuel system used with a turbojet engine

Date: August 19, 1957
Creator: Algranti, J. S.; Braithwaite, W. M. & Fenn, D. B.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Analysis of two-stage-turbine efficiency characteristics in terms of work and speed requirements

Analysis of two-stage-turbine efficiency characteristics in terms of work and speed requirements

Date: August 30, 1957
Creator: Stewart, Warner L & Wintucky, William T
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Approximate analysis of effects of large deflections and initial twist on torsional stiffness of a cantilever plate subjected to thermal stresses

Approximate analysis of effects of large deflections and initial twist on torsional stiffness of a cantilever plate subjected to thermal stresses

Date: August 1957
Creator: Heldenfels, Richard R & Vosteen, Louis F
Description: None
Contributing Partner: UNT Libraries Government Documents Department
A brief analog investigation of inertia coupling in rolling maneuvers of an airplane configuration using a variable-incidence wing as the longitudinal control

A brief analog investigation of inertia coupling in rolling maneuvers of an airplane configuration using a variable-incidence wing as the longitudinal control

Date: August 6, 1957
Creator: Gillis, Clarence L
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Compressive stress-strain properties of 17-7 PH and AM 350 stainless-steel sheet at elevated temperatures

Compressive stress-strain properties of 17-7 PH and AM 350 stainless-steel sheet at elevated temperatures

Date: August 1, 1957
Creator: Stein, Bland A
Description: None
Contributing Partner: UNT Libraries Government Documents Department
A correlation of results of a flight investigation with results of an analytical study of effects of wing flexibility on wing strains due to gusts

A correlation of results of a flight investigation with results of an analytical study of effects of wing flexibility on wing strains due to gusts

Date: August 1, 1957
Creator: Shufflebarger, C C; Payne, Chester B & Cahen, George L
Description: None
Contributing Partner: UNT Libraries Government Documents Department
The Design and Cascade Tests of Free-streamline and Full-contour 160 Deg Turning Supersonic-turbine-blade Sections

The Design and Cascade Tests of Free-streamline and Full-contour 160 Deg Turning Supersonic-turbine-blade Sections

Date: August 16, 1957
Creator: Westphal, W. R.
Description: Supersonic flow of two turbine blade sections with turning angle of 160-degrees.
Contributing Partner: UNT Libraries Government Documents Department
The design and cascade tests of free-streamline and full-contour 160 degrees turning supersonic-turbine-blade sections

The design and cascade tests of free-streamline and full-contour 160 degrees turning supersonic-turbine-blade sections

Date: August 16, 1957
Creator: Westphal, Willard R
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Design and performance of flight-type liquid-hydrogen heat exchanger

Design and performance of flight-type liquid-hydrogen heat exchanger

Date: August 19, 1957
Creator: Fenn, David B; Braithwaite, Willis M & Ordin, Paul M
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Design and performance of flight type liquid hydrogen heat exchanger

Design and performance of flight type liquid hydrogen heat exchanger

Date: August 19, 1957
Creator: Braithwaite, W. M.; Fenn, D. B. & Ordin, P. M.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Design and performance of fuel control for aircraft hydrogen fuel system

Design and performance of fuel control for aircraft hydrogen fuel system

Date: August 19, 1957
Creator: Otto, Edward W; HILLER KIRBY W & Ross, Phil S
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Design and performance of fuel control for aircraft hydrogen fuel system

Design and performance of fuel control for aircraft hydrogen fuel system

Date: August 19, 1957
Creator: Hiller, K. W.; Otto, E. W. & Ross, P. S.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
A discussion of cone and flat-plate Reynolds numbers for equal ratios of the laminar shear to the shear caused by small velocity fluctuations in a laminar boundary layer

A discussion of cone and flat-plate Reynolds numbers for equal ratios of the laminar shear to the shear caused by small velocity fluctuations in a laminar boundary layer

Date: August 1, 1957
Creator: Tetervin, Neal
Description: By use of the linear theory of boundary-layer stability and Schlichting's formula for the maximum amplification of a disturbance, an approximate relation is derived between the Reynolds number on a cone and the Reynolds number on a flat plate for equal closeness to transition. The indication is that the ratio of the cone Reynolds number for transition, based on the distance to the cone apex, to the plate Reynolds number for transition, based on the distance to the leading edge, is not in general equal to 3, as has been suggested by other investigators, but varies from 3 when transition occurs at the minimum critical Reynolds number to unity when transition occurs at a large multiple of the critical Reynolds number.
Contributing Partner: UNT Libraries Government Documents Department
Drop burning rates of hydrocarbon and nonhydrocarbon fuels

Drop burning rates of hydrocarbon and nonhydrocarbon fuels

Date: August 6, 1957
Creator: Smith, Arthur L & Graves, Charles C
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Effect of crystal orientation on fatigue-crack initiation in polycrystalline aluminum alloys

Effect of crystal orientation on fatigue-crack initiation in polycrystalline aluminum alloys

Date: August 1, 1957
Creator: Weinberg, J G & Bennett, J A
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Effect of nose shape on subsonic aerodynamic characteristics of a body of revolution having a fineness ratio of 10.94

Effect of nose shape on subsonic aerodynamic characteristics of a body of revolution having a fineness ratio of 10.94

Date: August 12, 1957
Creator: Polhamus, Edward C
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Effects of blade plan form on free-space oscillating pressures near propellers at flight Mach numbers to 0.72

Effects of blade plan form on free-space oscillating pressures near propellers at flight Mach numbers to 0.72

Date: August 1, 1957
Creator: Kurbjun, Max C
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Effects of control profile on the oscillating hinge-moment and flutter characteristics of a flap-type control at transonic speeds

Effects of control profile on the oscillating hinge-moment and flutter characteristics of a flap-type control at transonic speeds

Date: August 23, 1957
Creator: Moseley, William C , Jr & Price, George W , Jr
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Effects of internal-area distribution, spike translation, and throat boundary-layer control on performance of a double-cone axisymmetric inlet at Mach numbers from 3.0 to 2.0

Effects of internal-area distribution, spike translation, and throat boundary-layer control on performance of a double-cone axisymmetric inlet at Mach numbers from 3.0 to 2.0

Date: August 30, 1957
Creator: Conners, James F; Lovell, J Calvin & Wise, George A
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Effects of jet exhausts on flight-determined longitudinal and lateral dynamic stability characteristics of the Douglas D-558-II research airplane

Effects of jet exhausts on flight-determined longitudinal and lateral dynamic stability characteristics of the Douglas D-558-II research airplane

Date: August 23, 1957
Creator: Wolowicz, Chester H & Rediess, Herman A
Description: None
Contributing Partner: UNT Libraries Government Documents Department
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