WorldCat Identities

Ferri, Antonio 1912-

Overview
Works: 83 works in 216 publications in 2 languages and 1,263 library holdings
Genres: Periodicals  Conference papers and proceedings 
Roles: Author, Editor, Other
Publication Timeline
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Most widely held works about Antonio Ferri
 
Most widely held works by Antonio Ferri
Elements of aerodynamics of supersonic flows by Antonio Ferri( Book )

16 editions published between 1949 and 2005 in English and Undetermined and held by 281 WorldCat member libraries worldwide

Fundamental data obtained from shock-tube experiments by Antonio Ferri( Book )

12 editions published in 1961 in English and held by 210 WorldCat member libraries worldwide

Boundary layer problems by Antonio Ferri( )

13 editions published between 1962 and 2016 in English and held by 104 WorldCat member libraries worldwide

Progress in Aeronautical Sciences, Volume 3 provides information pertinent to the fundamental aspects of aerodynamics. This book covers a variety of topics related to the field of aerodynamics, including turbulence research, atmospheric velocity, hypersonic research, swept wing design, and ducted propellers. Organized into four chapters, this volume begins with an overview of the aerodynamics of swept-winged aircraft. This text then surveys the state of knowledge regarding the aerodynamics of ducted propellers. Other chapters consider hypersonic facilities and provide the reader with a
Proceedings of the conference on high-speed aeronautics, Polytechnic Institute of Brooklyn, January 20-22, 1955 by Polytechnic Institute of Brooklyn( Book )

11 editions published in 1955 in English and Undetermined and held by 88 WorldCat member libraries worldwide

Design and operation of intermittent supersonic wind tunnels by Antonio Ferri( Book )

6 editions published in 1954 in English and Multiple languages and held by 78 WorldCat member libraries worldwide

Selected papers on advanced design of air vehicles by Antonio Ferri( Book )

8 editions published between 1975 and 1977 in English and held by 52 WorldCat member libraries worldwide

This publication contains a selection of ten papers by Professor Antonio Ferri. They are published to bring together in one place examples of Professor Ferri's most important contributions to aerospace research and development. A biography of Professor Ferri is included, together with a bibliography of his works, and tributes from his friends and colleagues
Airframe/engine integration by North Atlantic Treaty Organization( Book )

4 editions published in 1972 in English and Undetermined and held by 46 WorldCat member libraries worldwide

Effect of premixing quality on oxides of nitrogen in gas turbine combustors by Gerald Roffe( Book )

4 editions published in 1976 in English and held by 34 WorldCat member libraries worldwide

Completed tabulation in the United States of tests of 24 airfoils at high Mach numbers (Derived from interrupted work at Guidonia, Italy in the 1.31- by 1.74-foot high-speed tunnel) by United States( )

5 editions published between 1045 and 1946 in English and held by 23 WorldCat member libraries worldwide

Two-dimensional data for 24 airfoil sections tested in the 1.31- by 1.74-foot high-speed tunnel at Guidonia, Italy, are presented. The test Mach numbers ranged from 0.40 to 0.94 and Reynolds numbers ranged from 340,000 to 420,000. The results indicate that thickness ratio is dominating shape parameter at high Mach numbers and that aerodynamic advantages are attainable by using thinnest possible sections
Supersonic-tunnel tests of projectiles in Germany and Italy by Antonio Ferri( )

3 editions published in 1945 in English and held by 20 WorldCat member libraries worldwide

Tests were performed in the Gottingen (Germany) and Guidonia (Italy) supersonic tunnels in order to determine the aerodynamic characteristics of projectiles of various shapes. The Mach numbers ranged from about 1.3 to 3.2 for the Gottingen tests and from 1.44 to 2.66 for the Guidonia tests. The results show that increasing the relative length of the nose causes the drag coefficient to decrease and the center of pressure to move forward. For a given length, the nose having minimum drag has a curved profile; the curvature is greatest at the tip and decreases to a very small value toward the rear of the nose, where the shape becomes approximately conical. As the Mach number increases, the drag coefficient decreases and the center of pressure moves toward the tail. For the higher Mach numbers the variation of the drag coefficient and the movement of the center of pressure are small. Existing aerodynamic theory gives values of the aerodynamic characteristics close to those determined experimentally for small flow deviations
Experimental verification of low sonic boom configuration by Antonio Ferri( Book )

3 editions published in 1972 in English and held by 20 WorldCat member libraries worldwide

Prevaporization and premixing to obtain low oxides of nitrogen in gas turbine combustors by Gerald Roffe( Book )

4 editions published in 1975 in English and held by 20 WorldCat member libraries worldwide

Progress in aeronautical sciences by Antonio Ferri( )

7 editions published between 1961 and 2014 in English and Undetermined and held by 18 WorldCat member libraries worldwide

Progress in aeronautical sciences( )

in English and held by 14 WorldCat member libraries worldwide

Application of the method of characteristics to supersonic rotational flow by Antonio Ferri( Book )

5 editions published between 1946 and 1949 in English and held by 13 WorldCat member libraries worldwide

A system for calculating the physical properties of supersonic rotational flow with axial symmetry and supersonic rotational flow in a two-dimensional field was determined by use of the characteristics method. The system was applied to the study of external and internal flow for supersonic inlets with axial symmetry. For a circular conical inlet became stronger as it approached the axis of the inlet and became a normal shock at the axis. The region for which strong shock occurred increased with the increase of the angle of internal cone at the lip of the inlet. For an inlet with a central body the method of characteristics was applied to the design of an internal-channel shape that, theoretically, results in very efficient recompression in the inlet; it was shown that if an effuser is connected with the diffuser a body of revolution with very small shock-wae drag can be determined
Improved nozzle testing techniques in transonic flow by North Atlantic Treaty Organization( Book )

4 editions published in 1975 in English and held by 10 WorldCat member libraries worldwide

Fundamental data obtained from shock-tube experiments( Book )

1 edition published in 1961 in English and held by 9 WorldCat member libraries worldwide

The hypersonic facility of the Polytechnic Institute of Brooklyn and its application to problems of hypersonic flight by Antonio Ferri( Book )

2 editions published in 1957 in English and held by 8 WorldCat member libraries worldwide

Preliminary investigation of a new type of supersonic inlet by Antonio Ferri( Book )

6 editions published between 1951 and 1952 in English and held by 8 WorldCat member libraries worldwide

A supersonic inlet with supersonic deceleration of the flow entirely outside of the inlet is considered. A particular arrangement with fixed geometry having a central body with a circular annular intake is analyzed, and it is shown theoretically that this arrangement gives high pressure recovery for a large range of Mach number and mass flow and therefore is practical for use on supersonic airplanes and missiles. For some Mach numbers the drag coefficient for this type of inlet is larger than the drag coefficient for the type of inlet with supersonic compression entirely inside, but the pressure recovery is larger for all flight conditions. The differences in drag can be eliminated for the design Mach number. Experimental results confirm the results of the theoretical analysis and show that pressure recoveries of 9% percent for Mach numbers of 1.33 and l.52, 92 percent for a Mach number of l.72, and 86 percent for a Mach number of 2.10 are possible with the configurations considered. If the mass flow decreases, the total drag coefficient increases gradually and the pressure recovery does not change appreciably. The results of this work were first presented in a classified document issued in l946
 
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Elements of aerodynamics of supersonic flows
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Alternative Names
Antonio Ferri ingénieur italien

Antonio Ferri Italiaans ruimteingenieur (1912-1975)

Antonio Ferri Italian scientist

Antonio Ferri italienischer Luft- und Raumfahrtingenieur

Ferri. A.

Ферри, Антонио

أنطونيو فيري

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