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 1.

A blade-element analysis for lifting rotors that is applicable for large inflow and blade angles and any reasonable blade geometry

作      者:Castles, Walter, Jr;New, Noah C
出版日期:1952
资源类型:科技报告
详细信息  原文下载:

 2.

A comparative examination of some measurements of airfoil section lift and drag at supercritical speeds

作      者:Crandall, Stewart M;Nitzberg, Gerald E
出版日期:1952
资源类型:科技报告
详细信息  原文下载:

 3.

A comparison of the experimental subsonic pressure distributions about several bodies of revolution with pressure distributions computed by means of the linearized theory

作      者:Matthews, Clarence W
出版日期:1952
资源类型:科技报告
详细信息  原文下载:

 4.

A comparison of the spanwise loading calculated by various methods with experimental loadings obtained on a 45 degrees sweptback wing of aspect ratio 8 at a Reynolds number of 4.0 x 10(exp 6)

作      者:Schneider, William C
出版日期:1952
资源类型:科技报告
详细信息  原文下载:

 5.

A comparison of two methods of linearized characteristics for a simple unsteady flow

作      者:Sullivan, Roger D
出版日期:1952
资源类型:科技报告
详细信息  原文下载:

 6.

A Correlation with Flight Tests of Results Obtained from the Measurement of Wing Pressure Distributions on a 1/4-scale Model of the X-1 Airplane (10-percent-thick Wing)

作      者:Runckel, Jack F;Henderson, James H
出版日期:1952
资源类型:科技报告
详细信息  原文下载:

 7.

A description and a comparison of certain nonlinear curve-fitting techniques, with applications to the analysis of transient-response data

作      者:Shinbrot, Marvin
出版日期:1952
资源类型:科技报告
详细信息  原文下载:

 8.

A Flight Investigation of the Effect of Shape and Thickness of the Boundary Layer on the Pressure Distribution in the Presence of Shock

作      者:Harrin, Eziaslav N
出版日期:1952
资源类型:科技报告
详细信息  原文下载:

 9.

A general theory of three-dimensional flow in subsonic and supersonic turbomachines of axial-, radial-, and mixed-flow types

作      者:Wu, Chung-Hua
出版日期:1952
资源类型:科技报告
详细信息  原文下载:

 10.

A low-speed experimental study of the directional characteristics of a sharp-nosed fuselage through a large angle-of-attack range at zero angle of sideslip

作      者:Letko, William
出版日期:1952
资源类型:科技报告
详细信息  原文下载:

 11.

A Low-speed Investigation of an Annular Transonic Air Inlet

作      者:Rinkoski, Donald W;Nichols, Mark R
出版日期:1952
资源类型:科技报告
详细信息  原文下载:

 12.

A Meter for Timing the Flow of Very Small Volumes of a Gas

作      者:Westmoreland, J C
出版日期:1952
资源类型:科技报告
详细信息  原文下载:

 13.

A method for estimating speed response of gas-turbine engines

作      者:Rosenzweig, Solomon;Gold, Harold
出版日期:1952
资源类型:科技报告
详细信息  原文下载:

 14.

A method for estimating the components of lift of wing-body combinations at supersonic speeds

作      者:Tucker, Warren A
出版日期:1952
资源类型:科技报告
详细信息  原文下载:

 15.

A method for finding a least-squares polynomial that passes through a specified point with specified derivatives

作      者:Tetervin, Neal
出版日期:1952
资源类型:科技报告
详细信息  原文下载:

 16.

A method for the determination of the time lag in pressure measuring systems incorporating capillaries

作      者:Robins, A Warner;Sinclair, Archibald R
出版日期:1952
资源类型:科技报告
详细信息  原文下载:

 17.

A method of selecting the thickness, hollowness, and size of a supersonic wing for least drag and sufficient bending strength at specified flight conditions

作      者:Amick, James L
出版日期:1952
资源类型:科技报告
详细信息  原文下载:

 18.

A Miniature Electrical Pressure Gage Utilizing a Stretched Flat Diagram

作      者:Patterson, John L
出版日期:1952
资源类型:科技报告
详细信息  原文下载:

 19.

A Preliminary Gust-tunnel Investigation of Leading-edge Separation on Swept Wings

作      者:Cahen, George L
出版日期:1952
资源类型:科技报告
详细信息  原文下载:

 20.

A preliminary investigation of shock-wave reflections in a small closed ballistic range with various types of walls

作      者:Sabol, A P
出版日期:1952
资源类型:科技报告
详细信息  原文下载:

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