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 1.

A Brief Hydrodynamic Investigation of a Navy Seaplane Design Equipped with a Hydro-ski

作      者:Hoffman, Edward L;Fisher, Lloyd J
出版日期:1953
资源类型:科技报告
详细信息  原文下载:

 2.

A collection of data for zero-lift damping in roll of wing-body combinations as determined with rocket-powered models equipped with roll-torque nozzles

作      者:Stone, David G
出版日期:1953
资源类型:科技报告
详细信息  原文下载:

 3.

A combined aerodynamic and guidance approach for a simple homing system

作      者:Gardiner, Robert A
出版日期:1953
资源类型:科技报告
详细信息  原文下载:

 4.

A comparison of gust loads measured in flight on a swept-wing airplane and an unswept-wing airplane

作      者:Mickleboro, Harry C;Funk, Jack
出版日期:1953
资源类型:科技报告
详细信息  原文下载:

 5.

A Comparison of Several Systems of Boundary-layer Removal Ahead of a Typical Conical External-compression Side Inlet at Mach Numbers of 1.88 and 2.93

作      者:Johnson, Harry W;Piercy, Thomas G
出版日期:1953
资源类型:科技报告
详细信息  原文下载:

 6.

A comparison of typical national gas turbine establishment and NACA axial-flow compressor blade sections in cascade at low speed

作      者:Emery, James C;Felix, A Richard
出版日期:1953
资源类型:科技报告
详细信息  原文下载:

 7.

A compilation of summaries from NACA reports on fuels research, 1945-1952

作      者:Dipiazza, J T
出版日期:1953
资源类型:科技报告
详细信息  原文下载:

 8.

A correlation by means of transonic similarity rules of the experimentally determined characteristics of 18 cambered wings of rectangular plan form

作      者:Mcdevitt, John B
出版日期:1953
资源类型:科技报告
详细信息  原文下载:

 9.

A Flight Comparison of a Submerged Inlet and a Scoop Inlet at Transonic Speeds

作      者:Rolls, L Stewart
出版日期:1953
资源类型:科技报告
详细信息  原文下载:

 10.

A Flight Investigation at Mach Numbers from 0.67 to 1.81 of the Longitudinal Stability and Control Characteristics of a 60 Degree Delta-wing Missile Configuration Having an All-movable Tail

作      者:Moul, Martin T;Baber, Hal T , Jr
出版日期:1953
资源类型:科技报告
详细信息  原文下载:

 11.

A flight investigation of some effects of automatic control on gust loads

作      者:Payne, Chester B
出版日期:1953
资源类型:科技报告
详细信息  原文下载:

 12.

A Flight Investigation of the Effect of Leading-edge Camber on the Aerodynamic Characteristics of a Swept-wing Airplane

作      者:Matteson, Frederick H;Anderson, Seth B;Van Dyke, Rudolph D , Jr
出版日期:1953
资源类型:科技报告
详细信息  原文下载:

 13.

A flight investigation of the effects of varied lateral damping on the effectiveness of a fighter airplane as a gun platform

作      者:Champine, Robert A;Kuehnel, Helmut A;Beckhardt, Arnold R
出版日期:1953
资源类型:科技报告
详细信息  原文下载:

 14.

A Flight Study of the Effects on Tracking Performance of Changes in the Lateral-oscillatory Characteristics of a Fighter Airplane

作      者:Mcneill, Walter E;Van Dyke, Rudolph D , Jr;Drinkwater, Fred J , III
出版日期:1953
资源类型:科技报告
详细信息  原文下载:

 15.

A Free-flight Investigation at Zero Lift in the Mach Number Range Between 0.7 and 1.4 to Determine the Effectiveness of an Inset Tab as a Means of Aerodynamically Relieving Aileron Hinge Moments

作      者:Bland, William M , Jr;Marley, Edward T
出版日期:1953
资源类型:科技报告
详细信息  原文下载:

 16.

A method for calculating the aerodynamic loading on wing-tip-tank combinations in subsonic flow

作      者:Zlotnick, Martin;Robinson, Samuel W , Jr
出版日期:1953
资源类型:科技报告
详细信息  原文下载:

 17.

A Method for Estimating the Rolling Moments Caused by Wing-tail Interference for Missiles at Supersonic Speeds

作      者:Hikido, Katsumi;Edwards, Sherman
出版日期:1953
资源类型:科技报告
详细信息  原文下载:

 18.

A Method of Calibrating Airspeed Installations on Airplanes at Transonic and Supersonic Speeds by the Use of Accelerometer and Attitude-Angle Measurements

作      者:Lina, Lindsay J;Trant, James P , Jr;Zalovick, John A
出版日期:1953
资源类型:科技报告
详细信息  原文下载:

 19.

A New Simple Interferometer for Obtaining Quantitatively Evaluable Flow Patterns

作      者:Erdmann, S F
出版日期:1953
资源类型:科技报告
详细信息  原文下载:

 20.

A note on the drag due to lift of delta wings at Mach numbers up to 2.0

作      者:Kelly, Thomas C;Osborne, Robert S
出版日期:1953
资源类型:科技报告
详细信息  原文下载:

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