The effects of propeller operation on the static longitudinal stability of single-engine tractor monoplanes are analyzed, and a simple method is presented for computing power-on pitching-moment curves for flap-retracted flight conditions. The methods evolved are based on the results of powered-model wind-tunnel investigations of 28 model configurations. Correlation curves are presented from which the effects of power on the downwash over the tail and the stabilizer effectiveness can be rapidly predicted. The procedures developed enable prediction of power-on longitudinal stability characteristics that are generally in very good agreement with experiment
A flight test has been conducted to determine the longitudinal stability and control characteristics...
The effects of power on the stability and the control characteristics of an airplane are discussed a...
Part 1 presents the results of a wind tunnel test of a biplane model with an 18 inch span. The lift,...
This report has three main purposes: 1. To establish an engineering computation procedure for pre...
This thesis is to be considered a continuation of the material presented in the paper by Dr. C. B. M...
A great majority of present day airplanes are of the low wing cantilever type. An investigation int...
Report presents the results of a study of data obtained in the NACA full-scale wind tunnel concernin...
To obtain the change in the longitudinal moment of a low winged monoplane caused by the addition of ...
Report presents the results of a study of data obtained in the NACA full-scale wind tunnel concernin...
The development and operation of increasingly powerful military turboprop training aircraft is re-in...
A comparison of the experimental results with those computed by use of existing theory is included. ...
A low-speed investigation was made of a 1/6-scale model of the Republic XF-84H airplane. The model h...
A low-speed investigation was made of a 1/6-scale model of the Republic XF-84H airplane. The model h...
Data obtained in the A? A. C. A. full-scale wind tunnel concerning the e~ects of interference and of...
A Four-Degree Of Freedom Model (Pitch, Yaw And Two Off The Propeller Plane Deformations From Blade F...
A flight test has been conducted to determine the longitudinal stability and control characteristics...
The effects of power on the stability and the control characteristics of an airplane are discussed a...
Part 1 presents the results of a wind tunnel test of a biplane model with an 18 inch span. The lift,...
This report has three main purposes: 1. To establish an engineering computation procedure for pre...
This thesis is to be considered a continuation of the material presented in the paper by Dr. C. B. M...
A great majority of present day airplanes are of the low wing cantilever type. An investigation int...
Report presents the results of a study of data obtained in the NACA full-scale wind tunnel concernin...
To obtain the change in the longitudinal moment of a low winged monoplane caused by the addition of ...
Report presents the results of a study of data obtained in the NACA full-scale wind tunnel concernin...
The development and operation of increasingly powerful military turboprop training aircraft is re-in...
A comparison of the experimental results with those computed by use of existing theory is included. ...
A low-speed investigation was made of a 1/6-scale model of the Republic XF-84H airplane. The model h...
A low-speed investigation was made of a 1/6-scale model of the Republic XF-84H airplane. The model h...
Data obtained in the A? A. C. A. full-scale wind tunnel concerning the e~ects of interference and of...
A Four-Degree Of Freedom Model (Pitch, Yaw And Two Off The Propeller Plane Deformations From Blade F...
A flight test has been conducted to determine the longitudinal stability and control characteristics...
The effects of power on the stability and the control characteristics of an airplane are discussed a...
Part 1 presents the results of a wind tunnel test of a biplane model with an 18 inch span. The lift,...