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
This report is an analysis of the maximum flight radii of typical large airplanes and a discussion o...
The text gives theoretical formulas from which is computed a table for the pressure of air on coming...
This report is a compilation of test data on airplane fuselages, nacelles, airship cars, seaplane fl...
This report is concerned with the derivation of a chart for estimating the absolute ceiling of an ai...
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 contains the derivation and the verification of formulae for predicting the speed range ...
This report presents general formulas for the determination of all major airplane performance charac...
A new method for the prediction of airplane performance in level and climbing flight, together with ...
Equations have been developed for the analysis of the performance of the ideal airplane, leading to ...
In this report charts are given showing the relation between time, velocities, and altitude for airp...
This report was prepared for the National Advisory Committee for Aeronautics in order to supply the ...
Symbols and definition of various airspeed terms that have been adopted as standard by the NACA subc...
Time-history data of airspeed, altitude, and acceleration obtained with the NACA VGH recorder from a...
This report was prepared at the request of the National Advisory Committee for Aeronautics in order ...
This report is an analysis of the maximum flight radii of typical large airplanes and a discussion o...
The text gives theoretical formulas from which is computed a table for the pressure of air on coming...
This report is a compilation of test data on airplane fuselages, nacelles, airship cars, seaplane fl...
This report is concerned with the derivation of a chart for estimating the absolute ceiling of an ai...
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 contains the derivation and the verification of formulae for predicting the speed range ...
This report presents general formulas for the determination of all major airplane performance charac...
A new method for the prediction of airplane performance in level and climbing flight, together with ...
Equations have been developed for the analysis of the performance of the ideal airplane, leading to ...
In this report charts are given showing the relation between time, velocities, and altitude for airp...
This report was prepared for the National Advisory Committee for Aeronautics in order to supply the ...
Symbols and definition of various airspeed terms that have been adopted as standard by the NACA subc...
Time-history data of airspeed, altitude, and acceleration obtained with the NACA VGH recorder from a...
This report was prepared at the request of the National Advisory Committee for Aeronautics in order ...
This report is an analysis of the maximum flight radii of typical large airplanes and a discussion o...
The text gives theoretical formulas from which is computed a table for the pressure of air on coming...
This report is a compilation of test data on airplane fuselages, nacelles, airship cars, seaplane fl...