Effect of thrust reverser operation on the lateral-directional characteristics of a three-surface F-15 model at transonic speeds View on Open Library

Effect of thrust reverser operation on the lateral-directional characteristics of a three-surface F-15 model at transonic speeds

by E. Ann Bare

No reviews yet
First published: 1983 1 language
Subjects
Jet nozzles Jet planes Thrust reversers

Reviews

Log in or sign up to write a review.

No reviews yet. Be the first!

More by E. Ann Bare

Effect of in-flight thrust reversing on vertical-tail loads of F-18 and F-15 airplane models

Effect of in-flight thrust reversing on ...

Flow field over the wing of a delta-wing fighter model with vortex control devices at Mach 0.6 to 1.2

Flow field over the wing of a delta-wing...

Static internal performance of a two-dimensional convergent-divergent nozzle with thrust vectoring

Static internal performance of a two-dim...

Static internal performance of convergent single-expansion-ramp nozzles with various combinations of internal geometric parameters

Static internal performance of convergen...

Investigation of installation effects on twin-engine convergent-divergent nozzles

Investigation of installation effects on...

You Might Also Like

More in Jet nozzles
Numerical method for predicting flow characteristics and performance of nonaxisymmetric nozzles

Numerical method for predicting flow cha...

P. D. Thomas
Boundary-layer separation on isolated boattail nozzles

Boundary-layer separation on isolated bo...

William Kelly Abeyounis
Introduction to molecular beams gas dynamics

Introduction to molecular beams gas dyna...

Giovanni Sanna
Effects of internal yaw-vectoring devices on the static performance of a pitch-vectoring nonaxisymmetric convergent-divergent nozzle

Effects of internal yaw-vectoring device...

Scott C. Asbury
Free jet feasibility study of a thermal acoustic shield concept for AST/VCE application

Free jet feasibility study of a thermal ...

B. A. Janardan
Static thrust-vectoring performance of nonaxisymmetric convergent-divergent nozzles with post-exit yaw vanes

Static thrust-vectoring performance of n...

Robert J. Foley