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 1.

A Balsa-dust Technique for Air-flow Visualization and Its Application to Flow Through Model Helicopter Rotors in Static Thrust

作      者:Taylor, Marion K
出版日期:1950
资源类型:科技报告
详细信息  原文下载:

 2.

A Comparison of the Aerodynamic Characteristics at Transonic Speeds of Four Wing-fuselage Configurations as Determined from Different Test Techniques

作      者:Myers, Boyd C , II;Mattson, Axel T;Donlan, Charles J
出版日期:1950
资源类型:科技报告
详细信息  原文下载:

 3.

A comparison of the lateral controllability with flap and plug ailerons on a sweptback-wing model

作      者:Stassi, Paul P;Lovell, Powell M , Jr
出版日期:1950
资源类型:科技报告
详细信息  原文下载:

 4.

A comparison of the lateral controllability with flap and plug ailerons on a sweptback-wing model having full-span flaps

作      者:Lovell, Powell M , Jr
出版日期:1950
资源类型:科技报告
详细信息  原文下载:

 5.

A comparison of theoretical and experimental wing bending moments during seaplane landings

作      者:Rodriguez, Jose L;Beck, Edgar B;Merten, Kenneth F
出版日期:1950
资源类型:科技报告
详细信息  原文下载:

 6.

A comparison of theory and experiment for high-speed free-molecule flow

作      者:Goodwin, Glen;Stalder, Jackson R;Creager, Marcus O
出版日期:1950
资源类型:科技报告
详细信息  原文下载:

 7.

A Description of the Design of Highly Swept Propeller Blades

作      者:Whitcomb, Richard T
出版日期:1950
资源类型:科技报告
详细信息  原文下载:

 8.

A Design Study of Leading-edge Inlets for Unswept Wings

作      者:Dannenberg, Robert E
出版日期:1950
资源类型:科技报告
详细信息  原文下载:

 9.

A Determination of the Laminar-, Transitional-, and Turbulent-boundary-layer Temperature-recovery Factors on a Flat Plate in Supersonic Flow

作      者:Stalder, Jackson R;Rubesin, Morris W;Tendeland, Thorval
出版日期:1950
资源类型:科技报告
详细信息  原文下载:

 10.

A Flight Investigation and Analysis of the Lateral-oscillation Characteristics of an Airplane

作      者:Stough, Carl J;Kauffman, William M
出版日期:1950
资源类型:科技报告
详细信息  原文下载:

 11.

A general integral form of the boundary-layer equation for incompressible flow with an application to the calculation of the separation point of turbulent boundary layers

作      者:Tetervin, Neal;Lin, Chia Chiao
出版日期:1950
资源类型:科技报告
详细信息  原文下载:

 12.

A method for predicting the low speed chordwise pressure distribution over sharp edge airfoil sections with plain flaps at the leading and trailing edges

作      者:Nuber, Robert J;Cahill, Jones F
出版日期:1950
资源类型:科技报告
详细信息  原文下载:

 13.

A method of calibrating airspeed installations on airplanes at transonic and supersonic speeds by use of accelerometer and attitude-angle measurements

作      者:Zalovcik, John A
出版日期:1950
资源类型:科技报告
详细信息  原文下载:

 14.

A method of computing subsonic flows around given airfoils

作      者:Gelbart, Abe;Resch, Daniel
出版日期:1950
资源类型:科技报告
详细信息  原文下载:

 15.

A numerical method for the stress analysis of stiffened-shell structures under nonuniform temperature distributions

作      者:Heldenfels, Richard R
出版日期:1950
资源类型:科技报告
详细信息  原文下载:

 16.

A numerical procedure for designing cascade blades with prescribed velocity distribution in incompressible potential flow

作      者:Hansen, Arthur G;Yohner, Peggy L
出版日期:1950
资源类型:科技报告
详细信息  原文下载:

 17.

A Preliminary Experimental and Analytical Evaluation of Diborane as a Ram-jet Fuel

作      者:Gammon, Benson E;Genco, Russell S;Gerstein, Melvin
出版日期:1950
资源类型:科技报告
详细信息  原文下载:

 18.

A Preliminary Flight Investigation of the Effects of Vortex Generators on Separation Due to Shock

作      者:Reed, Wilmer H , III;Lina, Lindsay J
出版日期:1950
资源类型:科技报告
详细信息  原文下载:

 19.

A preliminary investigation of wall effects on pressure-inflammability limits of propane-air mixtures

作      者:Belles, Frank E
出版日期:1950
资源类型:科技报告
详细信息  原文下载:

 20.

A pressure-distribution investigation of a supersonic-aircraft fuselage and calibration of the Mach number 1.40 nozzle of the Langley 4- by 4-foot supersonic tunnel

作      者:Hasel, Lowell E;Sinclair, Archibald R
出版日期:1950
资源类型:科技报告
详细信息  原文下载:

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