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  Partner: UNT Libraries Government Documents Department
 Collection: Technical Report Archive and Image Library
Results 15251 - 15260 of 17,421
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On the Flutter of Cylindrical Shells and Panels Moving in a Flow of Gas

On the Flutter of Cylindrical Shells and Panels Moving in a Flow of Gas

Date: September 1, 1958
Creator: Stepanov, R. D.
Description: The equations of shells are taken in the form of the general technical theory of shallow shells and shells of medium length. The aerodynamic forces acting on a shell are taken into account only as forces of excess pressure according to the formula proposed by A.A. Iliushin in reference 3.
Contributing Partner: UNT Libraries Government Documents Department
Ordinates and theoretical pressure-distribution data for NACA 6- and 6A-series airfoil sections with thicknesses from 2 to 21 and from 2 to 15 percent chord, respectively

Ordinates and theoretical pressure-distribution data for NACA 6- and 6A-series airfoil sections with thicknesses from 2 to 21 and from 2 to 15 percent chord, respectively

Date: September 1, 1958
Creator: Patterson, Elizabeth W & Braslow, Albert L
Description: None
Contributing Partner: UNT Libraries Government Documents Department
A phenomenological theory for the transient creep of metals at elevated temperatures

A phenomenological theory for the transient creep of metals at elevated temperatures

Date: September 1, 1958
Creator: Stowell, Elbridge Z
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Preliminary heat-transfer studies on two bodies of revolution at angle of attack at a Mach number of 3.12

Preliminary heat-transfer studies on two bodies of revolution at angle of attack at a Mach number of 3.12

Date: September 1, 1958
Creator: Sands, Norman & Jack, John R
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Procedure for calculating flutter at high supersonic speed including camber deflections, and comparison with experimental results

Procedure for calculating flutter at high supersonic speed including camber deflections, and comparison with experimental results

Date: September 1, 1958
Creator: Morgan, Homer G; Huckel, Vera & Runyan, Harry L
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Propellant vaporization as a criterion for rocket-engine design : calculations of chamber length to vaporize various propellants

Propellant vaporization as a criterion for rocket-engine design : calculations of chamber length to vaporize various propellants

Date: September 1, 1958
Creator: Priem, Richard J
Description: None
Contributing Partner: UNT Libraries Government Documents Department
The rate of fatigue-crack propagation in two aluminum alloys

The rate of fatigue-crack propagation in two aluminum alloys

Date: September 1, 1958
Creator: Mcevily, Arthur J , Jr & Illg, Walter
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Rate of reaction of gaseous fluorine with water vapor at 35 C

Rate of reaction of gaseous fluorine with water vapor at 35 C

Date: September 1, 1958
Creator: Slabey, Vernon A & Fletcher, Edward A
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Relationship of metal surfaces to heat-aging properties of adhesive bonds

Relationship of metal surfaces to heat-aging properties of adhesive bonds

Date: September 1, 1958
Creator: Black, J M & Blomquist, R F
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Relative motion in the terminal phase of interception of a satellite or a ballistic missile

Relative motion in the terminal phase of interception of a satellite or a ballistic missile

Date: September 1, 1958
Creator: Hord, Richard
Description: None
Contributing Partner: UNT Libraries Government Documents Department