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  Partner: UNT Libraries Government Documents Department
 Collection: Technical Report Archive and Image Library
Some effects of roll rate on the longitudinal stability characteristics of a cruciform missile configuration as determined from flight test for a Mach number range of 1.1 to 1.8

Some effects of roll rate on the longitudinal stability characteristics of a cruciform missile configuration as determined from flight test for a Mach number range of 1.1 to 1.8

Date: June 19, 1956
Creator: Barber, H. T., Jr. & Lundstrom, R. R.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Some effects of roll rate on the longitudinal stability characteristics of a cruciform missile configuration as determined from flight test for a Mach number range of 1.1. to 1.8

Some effects of roll rate on the longitudinal stability characteristics of a cruciform missile configuration as determined from flight test for a Mach number range of 1.1. to 1.8

Date: June 19, 1956
Creator: Lundstrom, Reginald R & Baber, Hal T , Jr
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Some Effects of Roll Rate on the Longitudinal Stability Characteristics of the Hughes Falcon Missile, ''C'' Configuration, for a Mach Number Range of 1.1 to 1.8 as Determined from Flight Test

Some Effects of Roll Rate on the Longitudinal Stability Characteristics of the Hughes Falcon Missile, ''C'' Configuration, for a Mach Number Range of 1.1 to 1.8 as Determined from Flight Test

Date: December 27, 1955
Creator: Baber, H. T., Jr. & Lundstrom, R. R.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Some effects of roughness on stagnation-point heat transfer at a Mach number of 2, a stagnation temperature of 3,530 F, and a Reynolds number of 2.5 x 10(exp 6) per foot

Some effects of roughness on stagnation-point heat transfer at a Mach number of 2, a stagnation temperature of 3,530 F, and a Reynolds number of 2.5 x 10(exp 6) per foot

Date: May 26, 1958
Creator: Strass, H Kurt & Tyner, Thomas W
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Some effects of side-wall modifications on the drag and pressure recovery of an NACA submerged inlet at transonic speeds

Some effects of side-wall modifications on the drag and pressure recovery of an NACA submerged inlet at transonic speeds

Date: February 15, 1952
Creator: Taylor, Robert A
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Some effects of small-scale flow disturbance on nozzle-burner flames

Some effects of small-scale flow disturbance on nozzle-burner flames

Date: September 1, 1956
Creator: Wong, Edgar L
Description: Laminar-like and brush-like propane-air flames were obtained when wire grids were used as turbulence generators in a 1/2-inch nozzle burner. The laminar-like flames for grid-disturbed flow had a slightly higher burning velocity than "true" laminar flames (no grid used). The brush-like flames were similar to those obtained with pipe turbulent flow. Their burning-velocity dependence on a "flow disturbance" Reynolds number compared favorably with that obtained for pipe turbulent flames. Hot-wire-anemometer equipment was used to measure the flow disturbance intensity in the cold flow with and without the grids in place.
Contributing Partner: UNT Libraries Government Documents Department
Some effects of solidity on turning through constant-thickness circular-arc guide vanes in axial annular flow

Some effects of solidity on turning through constant-thickness circular-arc guide vanes in axial annular flow

Date: August 24, 1951
Creator: Mankuta, Harry & Guentert, Donald C
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Some effects of spanwise aileron location and wing structural rigidity on the rolling effectiveness of 0.3-chord flap-type ailerons on a tapered wing having 63 degrees sweepback at the leading edge and NACA 64A005 airfoil sections

Some effects of spanwise aileron location and wing structural rigidity on the rolling effectiveness of 0.3-chord flap-type ailerons on a tapered wing having 63 degrees sweepback at the leading edge and NACA 64A005 airfoil sections

Date: June 22, 1951
Creator: Strass, H Kurt; Fields, E M & Schult, Eugene D
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Some effects of spoiler height, wing flexibility, and wing thickness on rolling effectiveness and drag of unswept wings at Mach numbers between 0.4 and 1.7

Some effects of spoiler height, wing flexibility, and wing thickness on rolling effectiveness and drag of unswept wings at Mach numbers between 0.4 and 1.7

Date: October 7, 1952
Creator: Fields, E M
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Some effects of stator cone angle and blade-tip leakage on 40 percent reaction turbine having rotor-blade caps

Some effects of stator cone angle and blade-tip leakage on 40 percent reaction turbine having rotor-blade caps

Date: March 23, 1949
Creator: English, Robert E; Mccready, Robert J & Mccready, John S
Description: An investigation of the effects of stator cone angle and tip leakage on turbine performance.
Contributing Partner: UNT Libraries Government Documents Department
Some effects of sweep and aspect ratio on the transonic flutter characteristics of a series of thin cantilever wings having a taper ratio of 0.6

Some effects of sweep and aspect ratio on the transonic flutter characteristics of a series of thin cantilever wings having a taper ratio of 0.6

Date: January 24, 1956
Creator: Unangst, John R & Jones, George W , Jr
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Some effects of sweep and thickness on the experimental downwash characteristics at transonic speeds of a series of highly tapered wings with an aspect ratio of 3 : transonic bump method

Some effects of sweep and thickness on the experimental downwash characteristics at transonic speeds of a series of highly tapered wings with an aspect ratio of 3 : transonic bump method

Date: February 16, 1956
Creator: Few, Albert G , Jr
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Some effects of system nonlinearities in the problem of aircraft flutter

Some effects of system nonlinearities in the problem of aircraft flutter

Date: October 1, 1955
Creator: Woolston, Donald S; Runyan, Harry L & Byrdsong, Thomas A
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Some effects of tail height and wing plan form on the static longitudinal stability characteristics of a small-scale model at high subsonic speeds

Some effects of tail height and wing plan form on the static longitudinal stability characteristics of a small-scale model at high subsonic speeds

Date: May 1, 1957
Creator: Few, Albert G , Jr & King, Thomas J , Jr
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Some effects of valve friction and shock stick friction on control quality in a helicopter with hydraulic-power control systems

Some effects of valve friction and shock stick friction on control quality in a helicopter with hydraulic-power control systems

Date: May 1, 1957
Creator: Brown, B Porter & REEDER JOHN P
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Some effects of vanes and of turbulence in two-dimensional wide-angle subsonic diffusers

Some effects of vanes and of turbulence in two-dimensional wide-angle subsonic diffusers

Date: June 1, 1958
Creator: Moore, Carl A , Jr & Kline, Stephen J
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Some effects of variations in several parameters including fluid density on the flutter speed of light uniform cantilever wings

Some effects of variations in several parameters including fluid density on the flutter speed of light uniform cantilever wings

Date: December 1, 1951
Creator: Woolston, Donald S & Castile, George E
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Some effects of varying the damping in pitch and roll on the flying qualities of a small single-rotor helicopter

Some effects of varying the damping in pitch and roll on the flying qualities of a small single-rotor helicopter

Date: January 1, 1952
Creator: Reeder, John P & Whitten, James B
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Some effects of wing fences on the lateral stability derivatives of a 60 degree delta wing oscillating continuously in yaw

Some effects of wing fences on the lateral stability derivatives of a 60 degree delta wing oscillating continuously in yaw

Date: July 11, 1956
Creator: Riley, Donald R
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Some effects of wing height on the vertical-tail pressure distributions of a complete model in sideslip at high subsonic speeds

Some effects of wing height on the vertical-tail pressure distributions of a complete model in sideslip at high subsonic speeds

Date: July 17, 1957
Creator: Few, Albert G , Jr & Alford, William J , Jr
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Some elementary principles of shell stress analysis with notes on the use of the shear center

Some elementary principles of shell stress analysis with notes on the use of the shear center

Date: March 1, 1939
Creator: Kuhn, Paul
Description: The analysis of various types of shell under combined bending and torsion is discussed. The calculation and the use of the shear center are touched upon as incidental problems. Twelve fully worked numerical examples are given in an appendix.
Contributing Partner: UNT Libraries Government Documents Department
Some Engineering Problems of the Panama Canal in Their Relation to Geology and Topography

Some Engineering Problems of the Panama Canal in Their Relation to Geology and Topography

Date: August 1915
Creator: MacDonald, Donald F.
Description: Report issued by the Bureau of Mines over issues encountered during construction of the Panama Canal. As stated in the introduction, "this report aims to discuss, from the viewpoint of the mining geologist, the bearing of topographic and geologic conditions on certain problems that arose in the construction of the Panama Canal" (p. 7). This report includes tables, maps, illustrations, and photographs.
Contributing Partner: UNT Libraries Government Documents Department
Some Essential Safety Factors in Tunneling

Some Essential Safety Factors in Tunneling

Date: 1941
Creator: Harrington, D. & Ash, S. H. (Simon Harry), b. 1889
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Some exact solutions of two-dimensional flows of compressible fluid with hodograph method

Some exact solutions of two-dimensional flows of compressible fluid with hodograph method

Date: February 1, 1953
Creator: Chang, Chien-Chien & O'Brien, Vivian
Description: None
Contributing Partner: UNT Libraries Government Documents Department