Theoretical and experimental analysis of low-drag supersonic inlets having a circular cross section and a central body at Mach numbers of 3.30, 2.75, and 2.45
By: by Antonio Ferri and Louis M. Nucci.
Contributors: Nucci, Louis M., joint author.
Publisher: U.S. Govt. Print. Off.
Published: 1955
Place of publication: Washington
Language: eng
Number of pages: 37
Subjects: Airplanes -- Turbojet engines.; Airplanes -- Ramjet engines -- Air intakes.
Notes: Bibliography: p. 37.
Cover title.