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 1.

:investigation of a 24-inch Shock-in-rotor Type Supersonic Compressor Designed for Simple Radial Equilibrium Behind Normal Shock

作      者:Hartmann, Melvin J;Lown, Harold
出版日期:1951
资源类型:科技报告
详细信息  原文下载:

 2.

A biharmonic relaxation method for calculating thermal stress in cooled irregular cylinders

作      者:Holms, Arthur G
出版日期:1951
资源类型:科技报告
详细信息  原文下载:

 3.

A Comparison of Predicted and Experimentally Determined Longitudinal Dynamic Responses of a Stabilized Airplane

作      者:Waugh, Merle G;Gore, Marvin R;Smaus, Louis, H
出版日期:1951
资源类型:科技报告
详细信息  原文下载:

 4.

A comparison of the calculated maximum-maneuver response characteristics of three air-to-air, beam-rider, guided missiles having different lift ratios

作      者:Matthews, Howard F;Stewart, Elwood C
出版日期:1951
资源类型:科技报告
详细信息  原文下载:

 5.

A Comparison of the Experimental and Theoretical Loading over Triangular Wings at Supersonic Speeds

作      者:Phelps, E Ray;Boyd, John W
出版日期:1951
资源类型:科技报告
详细信息  原文下载:

 6.

A Comparison of the Experimental and Theoretical Loading over Triangular Wings in Sideslip at Supersonic Speeds

作      者:Boyd, John W
出版日期:1951
资源类型:科技报告
详细信息  原文下载:

 7.

A comparison of the measured and predicted lateral oscillatory characteristics of a 35 degrees swept-wing fighter airplane

作      者:Cooper, George E;Mcneill, Walter E
出版日期:1951
资源类型:科技报告
详细信息  原文下载:

 8.

A Comparison of the Turbulent Boundary-layer Growth on an Unswept and a Swept Wing

作      者:Altman, John M;Hayter, Nora-Lee F
出版日期:1951
资源类型:科技报告
详细信息  原文下载:

 9.

A Comparison of Two Techniques Utilizing Rocket-propelled Vehicles for the Determination of the Damping-in-roll Derivative

作      者:Sandahl, Carl A;Stone, David G
出版日期:1951
资源类型:科技报告
详细信息  原文下载:

 10.

A correlation of experimental zero-lift drag of rectangular wings with symmetrical NACA 65-series airfoil sections by means of the transonic similarity law for wings of finite aspect ratio

作      者:Danforth, Edward C B
出版日期:1951
资源类型:科技报告
详细信息  原文下载:

 11.

A critical review of notch sensitivity in stress-rupture tests

作      者:Sachs, George;Brown, W F , Jr
出版日期:1951
资源类型:科技报告
详细信息  原文下载:

 12.

A flight evaluation of the longitudinal stability characteristics associated with the pitch-up of a swept-wing airplane in maneuvering flight at transonic speeds

作      者:Anderson, Seth B;Bray, Richard S
出版日期:1951
资源类型:科技报告
详细信息  原文下载:

 13.

A flight investigation of the effect of center-of-gravity location on gust loads

作      者:Binckley, Earle T;Funk, Jack
出版日期:1951
资源类型:科技报告
详细信息  原文下载:

 14.

A Flight Study of Requirements for Satisfactory Lateral Oscillatory Characteristics of Fighter Aircraft

作      者:Creer, Brent Y;Liddell, Charles J , Jr;Van Dyke, Rudolph D , Jr
出版日期:1951
资源类型:科技报告
详细信息  原文下载:

 15.

A general through-flow theory of fluid flow with subsonic or supersonic velocity in turbomachines of arbitrary hub and casing shapes

作      者:Wu, Chung-Hua
出版日期:1951
资源类型:科技报告
详细信息  原文下载:

 16.

A Graphical Method for Plotting Amplitude and Phase Angle of Transfer Functions of Dynamic Systems Without Factoring Polynomials

作      者:Smith, Earl F
出版日期:1951
资源类型:科技报告
详细信息  原文下载:

 17.

A least squares curve fitting method with applications to the calculation of stability coefficients from transient-response data

作      者:Shinbrot, Marvin
出版日期:1951
资源类型:科技报告
详细信息  原文下载:

 18.

A method for calculating stresses in torsion-box covers with cutouts

作      者:Rosecrans, Richard
出版日期:1951
资源类型:科技报告
详细信息  原文下载:

 19.

A Method for Predicting the Upwash Angles Induced at the Propeller Plane of a Combination of Bodies with an Upswept Wing

作      者:Yaggy, Paul F
出版日期:1951
资源类型:科技报告
详细信息  原文下载:

 20.

A method for the design of sweptback wings warped to produce specified flight characteristics at supersonic speeds

作      者:Tucker, Warren A
出版日期:1951
资源类型:科技报告
详细信息  原文下载:

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