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 1.

A Comparison of the Longitudinal Aerodynamic Characteristics at Mach Numbers up to 0.94 of Swept Back Wings Having NACA 4-digit or NACA 64A Thickness Distributions

作      者:Sutton, Fred B;Dickson, Jerald K
出版日期:1954
资源类型:科技报告
详细信息  原文下载:

 2.

A compilation of experimental flutter information

作      者:Cunningham, H J;Brown, Harvey H
出版日期:1954
资源类型:科技报告
详细信息  原文下载:

 3.

A Flight Evaluation of the Stability and Control of the X-4 Swept-wing Semitailless Airplane

作      者:Sadoff, Melvin;Crossfield, A Scott
出版日期:1954
资源类型:科技报告
详细信息  原文下载:

 4.

A Flight Investigation at Transonic Speeds and Small Angles of Attack of the Aerodynamic Characteristics of a Model Having a 45 Degree Sweptback Wing of Aspect Ratio 3 with an Naca 64A006 Airfoil Section

作      者:Holdaway, George H
出版日期:1954
资源类型:科技报告
详细信息  原文下载:

 5.

A Flight Investigation at Transonic Speeds of the Aerodynamic Characteristics of a Model Having a Thin Unswept Wing of Aspect Ratio 3.1

作      者:White, Maurice D
出版日期:1954
资源类型:科技报告
详细信息  原文下载:

 6.

A Flight Investigation of the Effects of Inclination of the Principal Axis of Inertia on the Dynamic Lateral Stability of the Republic XF-91 Airplane

作      者:Finch, Thomas W
出版日期:1954
资源类型:科技报告
详细信息  原文下载:

 7.

A flight investigation of the transonic area rule for a 52.5 degree sweptback wing-body configuration at Mach numbers between 0.8 and 1.6

作      者:Hoffman, Sherwood
出版日期:1954
资源类型:科技报告
详细信息  原文下载:

 8.

A flight study of compressibility effects on the gust loads of a 35 degree sweptback-wing airplane

作      者:Funk, Jack;Mickleboro, Harry C
出版日期:1954
资源类型:科技报告
详细信息  原文下载:

 9.

A flow calorimeter for determining combustion efficiency from residual enthalpy of exhaust gases

作      者:Hibbard, Robert R;Evans, Albert
出版日期:1954
资源类型:科技报告
详细信息  原文下载:

 10.

A Low-speed Investigation of the Aerodynamic, Control, and Hinge-moment Characteristics of Two Types of Controls and Balancing Tabs on a Large-scale Thin Delta-wing-fuselage Model

作      者:Fink, Marvin P;Cocke, Bennie W
出版日期:1954
资源类型:科技报告
详细信息  原文下载:

 11.

A method for designing low-drag nose-inlet--body combinations for operation at moderate supersonic speeds

作      者:Howell, Robert R
出版日期:1954
资源类型:科技报告
详细信息  原文下载:

 12.

A method for increasing the effectiveness of stabilizing surfaces at high supersonic Mach numbers

作      者:Mclellan, Charles H
出版日期:1954
资源类型:科技报告
详细信息  原文下载:

 13.

A Method of Measuring Jet Thrust of Turbojet Engines in Flight Installations

作      者:Fenn, David B;Sivo, Joseph N
出版日期:1954
资源类型:科技报告
详细信息  原文下载:

 14.

A Preliminary Flight Investigation of an Oil-flow Technique for Air-flow Visualization

作      者:Mungall, Robert G;Johnson, Harold I
出版日期:1954
资源类型:科技报告
详细信息  原文下载:

 15.

A Preliminary Investigation of the Pressure Recovery of Several Two-dimensional Supersonic Inlets at Mach Number of 2.01

作      者:Comenzo, Raymond J
出版日期:1954
资源类型:科技报告
详细信息  原文下载:

 16.

A Preliminary Investigation of the Use of Circulation Control to Increase the Lift of a 45 Degree Sweptback Wing by Suction Through Trailing-edge Slots

作      者:Cook, Woodrow L;Hickey, David H;Griffin, Roy N JR
出版日期:1954
资源类型:科技报告
详细信息  原文下载:

 17.

A Preliminary Study of the Preparation of Slurry Fuels from Vaporized Magnesium

作      者:Walsh, Thomas J;Witzke, Walter R;Prok, George M
出版日期:1954
资源类型:科技报告
详细信息  原文下载:

 18.

A Study of the Characteristics of Human-Pilot Control Response to Simulated Aircraft Lateral Motions

作      者:Cheatham, Donald C
出版日期:1954
资源类型:科技报告
详细信息  原文下载:

 19.

A Study of the Radiation from Laminar and Turbulent Open Propane-air Flames as a Function of Flame Area, Equivalence Ratio, and Fuel Flow Rate

作      者:Bittker, David A;Clark, Thomas P
出版日期:1954
资源类型:科技报告
详细信息  原文下载:

 20.

A study of the use of controls and the resulting airplane response during service training operations of four jet fighter airplanes

作      者:Hamer, Harold A;Mayer, John P;Huss, Carl R
出版日期:1954
资源类型:科技报告
详细信息  原文下载:

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