Add to ORKGThis report contains the derivation and the verification of formulae for predicting the speed range ratio, the initial rate of climb, and the absolute ceiling of an airplane. Curves used in the computation are given in NACA-TR-171. Standard formulae for service ceiling, time of climb, cruising range, and endurance are also given in the conventional forms
While the reliability of predictions is poor the author still attempts to gauge the future speeds of...
This note is concerned with the effect of power on landing speed and apparent maximum lift coefficie...
The reliability of the assumption of a parabolic shape of the polar curve is investigated and found ...
This report contains a series of charts which were developed in order to simplify the estimation of ...
This report presents general formulas for the determination of all major airplane performance charac...
This report contains the derivation and the verification of formulae for predicting the speed range ...
This report develops new equations which give the range and endurance of airplanes with an accuracy ...
The aeronautical engineer often has occasion to estimate the absolute ceiling of an airplane for whi...
This report is concerned with the derivation of a chart for estimating the absolute ceiling of an ai...
This report is an analysis of the maximum flight radii of typical large airplanes and a discussion o...
A new method for the prediction of airplane performance in level and climbing flight, together with ...
This report contains a brief study of the variation of engine power with temperature and pressure. T...
The consistent increase in flying speed is perhaps th ~ most outstanding feature of modern aircraft ...
A study was made of the most important factors affecting the range of airplanes. Numerical examples ...
An investigation is made of the possible improvements in maximum, cruising, and climbing speeds atta...
While the reliability of predictions is poor the author still attempts to gauge the future speeds of...
This note is concerned with the effect of power on landing speed and apparent maximum lift coefficie...
The reliability of the assumption of a parabolic shape of the polar curve is investigated and found ...
This report contains a series of charts which were developed in order to simplify the estimation of ...
This report presents general formulas for the determination of all major airplane performance charac...
This report contains the derivation and the verification of formulae for predicting the speed range ...
This report develops new equations which give the range and endurance of airplanes with an accuracy ...
The aeronautical engineer often has occasion to estimate the absolute ceiling of an airplane for whi...
This report is concerned with the derivation of a chart for estimating the absolute ceiling of an ai...
This report is an analysis of the maximum flight radii of typical large airplanes and a discussion o...
A new method for the prediction of airplane performance in level and climbing flight, together with ...
This report contains a brief study of the variation of engine power with temperature and pressure. T...
The consistent increase in flying speed is perhaps th ~ most outstanding feature of modern aircraft ...
A study was made of the most important factors affecting the range of airplanes. Numerical examples ...
An investigation is made of the possible improvements in maximum, cruising, and climbing speeds atta...
While the reliability of predictions is poor the author still attempts to gauge the future speeds of...
This note is concerned with the effect of power on landing speed and apparent maximum lift coefficie...
The reliability of the assumption of a parabolic shape of the polar curve is investigated and found ...