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  Partner: UNT Libraries Government Documents Department
 Decade: 1950-1959
 Year: 1958
 Serial/Series Title: NACA Technical Notes
 Collection: National Advisory Committee for Aeronautics Collection
Accelerations in transport-airplane crashes

Accelerations in transport-airplane crashes

Date: February 1958
Creator: Preston, G Merritt & Pesman, Gerard J
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Acoustic, thrust, and drag characteristics of several full-scale noise suppressors for turbojet engines

Acoustic, thrust, and drag characteristics of several full-scale noise suppressors for turbojet engines

Date: April 1958
Creator: Ciepluch, Carl C; North, Warren J; Coles, Willard D & Antl, Robert J
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Aerodynamic Effects Caused by Icing of an Unswept NACA 65A004 Airfoil

Aerodynamic Effects Caused by Icing of an Unswept NACA 65A004 Airfoil

Date: February 1, 1958
Creator: Gray, Vernon H. & vonGlahn, Uwe H.
Description: The effects of ice formations on the section lift, drag, and pitching-moment coefficients of an unswept NACA 65A004 airfoil section of 6-foot chord were studied.. The magnitude of the aerodynamic penalties was primarily a function of the shape and size of the ice formation near the leading edge of the airfoil. The exact size and shape of the ice formations were determined photographically and found to be complex functions of the operating and icing conditions. In general, icing of the airfoil at angles of attack less than 40 caused large increases in section drag coefficients (as much as 350 percent in 8 minutes of heavy glaze icing), reductions in section lift coefficients (up to 13 percent), and changes in the pitching-moment coefficient from diving toward climbing moments. At angles of attack greater than 40 the aerodynamic characteristics depended mainly on the ice type. The section drag coefficients generally were reduced by the addition of rime ice (by as much as 45 percent in 8 minutes of icing). In glaze icing, however, the drag increased at these angles of attack. The section lift coefficients were variably affected by rime-ice formations; however, in glaze icing, lift increases at high angles of attack ...
Contributing Partner: UNT Libraries Government Documents Department
Analysis of harmonic forces produced at hub by imbalances in helicopter rotor blades

Analysis of harmonic forces produced at hub by imbalances in helicopter rotor blades

Date: April 1, 1958
Creator: Morduchow, M & Muzyka, A
Description: None
Contributing Partner: UNT Libraries Government Documents Department
An Analysis of Ramjet Engines Using Supersonic Combustion

An Analysis of Ramjet Engines Using Supersonic Combustion

Date: September 1, 1958
Creator: Weber, Richard J & Mackay, John S
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Analysis of stresses and deflections in a disk subjected to gyroscopic forces

Analysis of stresses and deflections in a disk subjected to gyroscopic forces

Date: March 1, 1958
Creator: Hirschberg, M H & Mendelson, A
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Analysis of the creep behavior of a square plate loaded in edge compression

Analysis of the creep behavior of a square plate loaded in edge compression

Date: September 1, 1958
Creator: Mccomb, Harvey G , Jr
Description: None
Contributing Partner: UNT Libraries Government Documents Department
An analysis of the optimization of a beam rider missile system

An analysis of the optimization of a beam rider missile system

Date: March 1, 1958
Creator: Shinbrot, Marvin & Carpenter, Grace C
Description: None
Contributing Partner: UNT Libraries Government Documents Department
An analysis of the turbulent boundary-layer characteristics on a flat plate with distributed light-gas injection

An analysis of the turbulent boundary-layer characteristics on a flat plate with distributed light-gas injection

Date: February 1, 1958
Creator: Rubesin, Morris W & Pappas, Constantine C
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Analysis of turbulent flow and heat transfer in noncircular passages

Analysis of turbulent flow and heat transfer in noncircular passages

Date: September 1, 1958
Creator: Deissler, Robert G & Taylor, Maynard F
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Analysis of turbulent flow and heat transfer on a flat plate at high Mach numbers with variable fluid properties

Analysis of turbulent flow and heat transfer on a flat plate at high Mach numbers with variable fluid properties

Date: April 1, 1958
Creator: Deissler, R G & Loeffler, A L , Jr
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Analytical and experimental investigation of aerodynamic forces and moments on low-aspect-ratio wings undergoing flapping oscillations

Analytical and experimental investigation of aerodynamic forces and moments on low-aspect-ratio wings undergoing flapping oscillations

Date: August 1, 1958
Creator: Woolston, Donald S; Clevenson, Sherman A & Leadbetter, Sumner A
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Analytical and experimental investigation of temperature recovery factors for fully developed flow of air in a tube

Analytical and experimental investigation of temperature recovery factors for fully developed flow of air in a tube

Date: September 1, 1958
Creator: Weiland, W F; Lowdermilk, W H & Deissler, R G
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Analytical investigation of acceleration restriction in a fighter airplane with an automatic control system

Analytical investigation of acceleration restriction in a fighter airplane with an automatic control system

Date: January 1, 1958
Creator: Matthews, James T , Jr
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Analytical relation for wake momentum thickness and diffusion ratio for low-speed compressor

Analytical relation for wake momentum thickness and diffusion ratio for low-speed compressor

Date: August 1, 1958
Creator: Lieblein, Seymour
Description: None
Contributing Partner: UNT Libraries Government Documents Department
An analytical study of turbulent and molecular mixing in rocket combustion

An analytical study of turbulent and molecular mixing in rocket combustion

Date: September 1, 1958
Creator: Bittker, David A
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Application of a high-temperature static strain gage to the measurement of thermal stresses in a turbine stator vane

Application of a high-temperature static strain gage to the measurement of thermal stresses in a turbine stator vane

Date: March 1, 1958
Creator: Kemp, R H; Morse, C R & Hirschberg, M H
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Application of statistical theory to beam-rider guidance in the presence of noise II : modified Wiener filter theory

Application of statistical theory to beam-rider guidance in the presence of noise II : modified Wiener filter theory

Date: June 1, 1958
Creator: Stewart, Elwood C
Description: None
Contributing Partner: UNT Libraries Government Documents Department
An approach to the problem of estimating severe and repeated gust    loads for missile operations

An approach to the problem of estimating severe and repeated gust loads for missile operations

Date: September 1, 1958
Creator: Press, Harry & Steiner, Roy
Description: None
Contributing Partner: UNT Libraries Government Documents Department
An approximate analytical method for studying entry into planetary atmospheres

An approximate analytical method for studying entry into planetary atmospheres

Date: May 1, 1958
Creator: Chapman, Dean R
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Approximate method for calculating motions in angles of attack and sideslip due to step pitching- and yawing-moment inputs during steady roll

Approximate method for calculating motions in angles of attack and sideslip due to step pitching- and yawing-moment inputs during steady roll

Date: September 1, 1958
Creator: Moul, Martin T & Brennan, Teresa R
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Approximate method for calculation of laminar boundary layer with heat transfer on a cone at large angle of attack in supersonic flow

Approximate method for calculation of laminar boundary layer with heat transfer on a cone at large angle of attack in supersonic flow

Date: September 1, 1958
Creator: Brunk, William E
Description: None
Contributing Partner: UNT Libraries Government Documents Department
An approximate method for design or analysis of two-dimensional subsonic-flow passages

An approximate method for design or analysis of two-dimensional subsonic-flow passages

Date: April 1, 1958
Creator: Valentine, E Floyd
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Approximate solutions of a class of similarity equations for three-dimensional, laminar, incompressible boundary-layer flows

Approximate solutions of a class of similarity equations for three-dimensional, laminar, incompressible boundary-layer flows

Date: September 1, 1958
Creator: Hansen, Arthur G & Herzig, Howard Z
Description: None
Contributing Partner: UNT Libraries Government Documents Department
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