Parametric investigation of single-expansion-ramp nozzles at Mach numbers from 0.60 to 1.20 /

Saved in:

Bibliographic Details
Main Author:	Capone, Francis J.
Corporate Author:	United States. National Aeronautics and Space Administration. Scientific and Technical Information Program
Other Authors:	Re, Richard J., Bare, E. Ann
Format:	Government Document Book
Language:	English
Published:	[Washington, D.C.] : [Springfield, Va.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [For sale by the National Technical Information Service], 1992.
Series:	NASA technical paper ; 3240.
Subjects:	Aerodynamics. Nozzles. Aerodynamic coefficients. Aerodynamic drag. Convergent nozzles. Convergent-divergent nozzles. Mach number. Nozzle design. Nozzle flow. Propulsion system performance. Wind tunnel tests.

Parametric investigation of single-expansion-ramp nozzles at Mach numbers from 0.60 to 1.20 by Capone, Francis J.

[Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [For sale by the National Technical Information Service], 1992

Format: Government Document Book

Parametric investigation of single-expansion-ramp nozzles at Mach numbers from 0.60 to 1.20 by Capone, Francis J.

[Washington, DC] : [Springfield, Va. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; For sale by the National Technical Information Service], 1992

Format: Government Document Book

Parametric investigation of single-expansion-ramp nozzles at Mach numbers from 0.60 to 1.20 /

Parametric investigation of single-expansion-ramp nozzles at Mach numbers from 0.60 to 1.20 by Capone, Francis J.

Parametric investigation of single-expansion-ramp nozzles at Mach numbers from 0.60 to 1.20 by Capone, Francis J.

Similar Items