Following the description of the new propulsion system and the definition of the propulsive efficiency, this efficiency is calculated under various conditions of flight with allowance for all internal losses. The efficiency and consumption curves are plotted, their practical values discussed and the behavior of the system analyzed at various altitudes and speeds. The immediate possibilities of the new system in flight at high and very high altitudes in relation to the theoretical and experimental results are discussed in detail
The focus of interest is the maneuvering flight of advanced entry vehicles operating at altitudes ab...
Results are presented for tests of two wings, an NACA 230-series wing and a highly-cambered NACA 66-...
An analysis is made of the stability of an airplane with ailerons free, with particular attention to...
A study was made of the most important factors affecting the range of airplanes. Numerical examples ...
The first part of this report details the efficiency and economy of airship travel, while the second...
A series of charts is given showing the variation of the velocity gained and the altitude lost in di...
This report is an analysis of the maximum flight radii of typical large airplanes and a discussion o...
A nondimensional economic examination of a parametrically-derived set of supersonic transport aircra...
Lift (L) and drag (D) characteristics have been obtained in flight for the X-29A airplane (a forward...
The zero and low speed controllability of heavy lift airships under various wind conditions as affec...
Comparing the results of the calculations for computing the mean pressure of an aviation engine for ...
This investigation was made to determine the pressure distribution over a rib of the wing and over a...
An empirical method is given for estimating the aerodynamic effect of ordinary and split flaps on ai...
The air forces on a systematic series of biplane and triplane cellule models are the subject of this...
An analytical investigation was made of the performance of isolated ram-jet engines in the flight Ma...
The focus of interest is the maneuvering flight of advanced entry vehicles operating at altitudes ab...
Results are presented for tests of two wings, an NACA 230-series wing and a highly-cambered NACA 66-...
An analysis is made of the stability of an airplane with ailerons free, with particular attention to...
A study was made of the most important factors affecting the range of airplanes. Numerical examples ...
The first part of this report details the efficiency and economy of airship travel, while the second...
A series of charts is given showing the variation of the velocity gained and the altitude lost in di...
This report is an analysis of the maximum flight radii of typical large airplanes and a discussion o...
A nondimensional economic examination of a parametrically-derived set of supersonic transport aircra...
Lift (L) and drag (D) characteristics have been obtained in flight for the X-29A airplane (a forward...
The zero and low speed controllability of heavy lift airships under various wind conditions as affec...
Comparing the results of the calculations for computing the mean pressure of an aviation engine for ...
This investigation was made to determine the pressure distribution over a rib of the wing and over a...
An empirical method is given for estimating the aerodynamic effect of ordinary and split flaps on ai...
The air forces on a systematic series of biplane and triplane cellule models are the subject of this...
An analytical investigation was made of the performance of isolated ram-jet engines in the flight Ma...
The focus of interest is the maneuvering flight of advanced entry vehicles operating at altitudes ab...
Results are presented for tests of two wings, an NACA 230-series wing and a highly-cambered NACA 66-...
An analysis is made of the stability of an airplane with ailerons free, with particular attention to...