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  Partner: UNT Libraries Government Documents Department
 Decade: 1950-1959
 Serial/Series Title: NACA Technical Memorandums
Flight experiences and tests on two airplanes with suction slots

Flight experiences and tests on two airplanes with suction slots

Date: January 1, 1950
Creator: Stueper, BY
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Development of a laminar boundary layer behind a suction point

Development of a laminar boundary layer behind a suction point

Date: March 1, 1952
Creator: Wuest, W.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
NACA Conference on High-Speed Aerodynamics  A compilation of papers presented

NACA Conference on High-Speed Aerodynamics A compilation of papers presented

Date: January 1, 1958
Creator: unknown
Description: None
Contributing Partner: UNT Libraries Government Documents Department
NACA Conference on Aircraft Loads, Structures, and Flutter

NACA Conference on Aircraft Loads, Structures, and Flutter

Date: March 5, 1957
Creator: unknown
Description: This document contains reproductions of technical papers on some of the most recent research results on aircraft loads, flutter, and structures from the NACA laboratories. These papers were presented by members of the staff of the NACA laboratories at the Conference held at the Langley Aeronautical Laboratory March 5, 6, and 7, 1957. The primary purpose of this Conference was to convey to contractors of the military services and others concerned with the design of aircraft these recent research results and to provide those attending an opportunity to discuss the results. The papers in this document are in the same form in which they were presented at the Conference in order to facilitate their prompt distribution. The original presentation and this record are considered as complementary to, rather than as substitutes for, the Committee?s more complete and formal reports. Accordingly, if information from this document is utilized it is requested that this document not be listed as a reference. Individual reports dealing with most of the information presented at the Conference will subsequently be published by NACA and will therefore be suitable as reference material.
Contributing Partner: UNT Libraries Government Documents Department
NACA Conference on Aerodynamics of High Speed Aircraft

NACA Conference on Aerodynamics of High Speed Aircraft

Date: November 1, 1955
Creator: unknown
Description: This document contains reproductions of technical papers presented by staff members of the NACA Laboratories at the NACA Conference on Aerodynamics of High-Speed Aircraft held at the Langley Aeronautical Laboratory November 1, 2, and 3, 1955. The primary purpose of the conference was to convey to contractors of the military services and others concerned with the design of aircraft the results of recent research and to provide those attending with an opportunity to discuss these results. The papers in this document are in the same form in which they were orally presented at the conference to facilitate their prompt distribution. The original presentation and this record are considered as complementary to, rather than as substitutes for, the Committee's more complete and formal reports.
Contributing Partner: UNT Libraries Government Documents Department
On the design of airfoils in which the transition of the boundary layer is delayed

On the design of airfoils in which the transition of the boundary layer is delayed

Date: October 1, 1952
Creator: Tani, I.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
NACA Conference on engine stall and surge

NACA Conference on engine stall and surge

Date: February 3, 1955
Creator: unknown
Description: None
Contributing Partner: UNT Libraries Government Documents Department
On the three-dimensional instability of laminar boundary layers on concave walls, Ph.D. Thesis - Goettingen Univ.

On the three-dimensional instability of laminar boundary layers on concave walls, Ph.D. Thesis - Goettingen Univ.

Date: June 1, 1954
Creator: Goertler, H.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Investigation of an Afterburning Ramjet Using Gaseous Hydrogen as Fuel at Mach Number of 3.0

Investigation of an Afterburning Ramjet Using Gaseous Hydrogen as Fuel at Mach Number of 3.0

Date: June 17, 1957
Creator: Wasserbauer, J. F.
Description: Afterburning ramjet using hydrogen at mach 3.0.
Contributing Partner: UNT Libraries Government Documents Department
On stability and turbulence of fluid flows

On stability and turbulence of fluid flows

Date: June 1, 1951
Creator: Heisenberg, Werner
Description: This investigation is divided into two parts, the treatment of the stability problem of fluid flows on the one hand, and that of the turbulent motion on the other. The first part summarizes all previous investigations under a unified point of view, that is, sets up as generally as possible the conditions under which a profile possesses unstable or stable characteristics, and indicates the methods for solution of the stability equation for any arbitrary velocity profile and for calculation of the critical Reynolds number for unstable profiles. In the second part, under certain greatly idealizing assumptions, differential equations for the turbulent motions are derived and from them qualitative information about several properties of the turbulent velocity distribution is obtained.
Contributing Partner: UNT Libraries Government Documents Department
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