Static internal performance characteristics of two thrust-reverser concepts for axisymmetric nozzles View on Open Library

Static internal performance characteristics of two thrust-reverser concepts for axisymmetric nozzles

by Laurence D. Leavitt

No reviews yet
First published: 1982 1 language
Subjects
Jet planes Thrust reversers Mathematical models Testing

Reviews

Log in or sign up to write a review.

No reviews yet. Be the first!

More by Laurence D. Leavitt

Effects of twin-vertical-tail parameters on twin-engine afterbody/nozzle aerodynamic characteristics

Effects of twin-vertical-tail parameters...

Longitudinal aerodynamic characteristics of a vectored-engine-over-wing configuration at subsonic speeds

Longitudinal aerodynamic characteristics...

Performance characteristics of axisymmetric convergent-divergent exhaust nozzles with longitudinal slots in the divergent flaps

Performance characteristics of axisymmet...

Effects of spanwise nozzle geometry and location on the longitudinal aerodynamic characteristics of a vectored-engine-over-wing configuration at subsonic speeds

Effects of spanwise nozzle geometry and ...

Effects of twin-vertical-tail parameters on twin-engine afterbody/nozzle aerodynamic characteristics

Effects of twin-vertical-tail parameters...

Performance characteristics of axisymmetric convergent-divergent exhaust nozzles with longitudinal slots in the divergent flaps

Performance characteristics of axisymmet...

You Might Also Like

More in Jet planes
Air pollution

Air pollution

United States. General Accounting Office
Defense acquisitions

Defense acquisitions

United States. General Accounting Office
Navy aviation

Navy aviation

United States. General Accounting Office
Contract pricing

Contract pricing

United States. General Accounting Office
Seedlings

Seedlings

Kate Riggs
F-22 aircraft

F-22 aircraft

United States. General Accounting Office