This report develops new equations which give the range and endurance of airplanes with an accuracy equal to that obtained from a step-by-step integration of the flight. A method of obtaining equally satisfactory results from Brequet's equations is also given in detail. A third method of calculating range and endurance, derived by the writer for use in routine estimating in the Bureau of Aeronautics, is also given in full. The reports contains tables and curves arranged for convenient use and illustrates the three methods by comparative estimates
Rules and methods for insuring safe structural strength of racing airplanes used in the major air me...
This report shows how the actual performance of an airplane varies with air temperature when the pre...
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 ...
This report contains the derivation and the verification of formulae for predicting the speed range ...
Equations have been developed for the analysis of the performance of the ideal airplane, leading to ...
This report presents general formulas for the determination of all major airplane performance charac...
A study was made of the most important factors affecting the range of airplanes. Numerical examples ...
A new method for the prediction of airplane performance in level and climbing flight, together with ...
The aeronautical engineer often has occasion to estimate the absolute ceiling of an airplane for whi...
This report is an analysis of the maximum flight radii of typical large airplanes and a discussion o...
In the present report the computation is actually carried through for the case of parallel spars of ...
This report is based upon an analysis of a large number of airplane-engine tests. It contains the re...
This investigation, which is a continuation of Technical Report 154, follows very closely the earlie...
This report is concerned with the derivation of a chart for estimating the absolute ceiling of an ai...
Rules and methods for insuring safe structural strength of racing airplanes used in the major air me...
This report shows how the actual performance of an airplane varies with air temperature when the pre...
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 ...
This report contains the derivation and the verification of formulae for predicting the speed range ...
Equations have been developed for the analysis of the performance of the ideal airplane, leading to ...
This report presents general formulas for the determination of all major airplane performance charac...
A study was made of the most important factors affecting the range of airplanes. Numerical examples ...
A new method for the prediction of airplane performance in level and climbing flight, together with ...
The aeronautical engineer often has occasion to estimate the absolute ceiling of an airplane for whi...
This report is an analysis of the maximum flight radii of typical large airplanes and a discussion o...
In the present report the computation is actually carried through for the case of parallel spars of ...
This report is based upon an analysis of a large number of airplane-engine tests. It contains the re...
This investigation, which is a continuation of Technical Report 154, follows very closely the earlie...
This report is concerned with the derivation of a chart for estimating the absolute ceiling of an ai...
Rules and methods for insuring safe structural strength of racing airplanes used in the major air me...
This report shows how the actual performance of an airplane varies with air temperature when the pre...
This report contains the derivation and the verification of formulae for predicting the speed range ...