Influence of base modifications on in-flight base drag in the presence of jet exhaust for Mach numbers from 0.7 to 1.5

View on Open Library

Influence of base modifications on in-flight base drag in the presence of jet exhaust for Mach numbers from 0.7 to 1.5

by Sheryll Goecke Powers

No reviews yet

First published: 1988 1 language

Subjects

Aerodynamics

Reviews

Log in or sign up to write a review.

No reviews yet. Be the first!

More by Sheryll Goecke Powers

Flight-measured pressure characteristics of aft-facing steps in high Reynolds number flow at Mach numbers of 2.20, 2.50, and 2.80 and comparison with other data

Flight-measured pressure characteristics...

Flight and wind-tunnel measurements showing base drag reduction provided by a trailing disk for high Reynolds number turbulent flow for subsonic and transonic Mach numbers

Flight and wind-tunnel measurements show...

Flight wing surface pressure and boundary-layer data report from the F-111 smooth variable-camber supercritical mission adaptive wing

Flight wing surface pressure and boundar...

Flight-measured pressure characteristics of aft-facing steps in high Reyonlds number flow at Mach numbers of 2.20, 2.50, and 2.80 and comparison with other data

Flight-measured pressure characteristics...

Women in flight research at NASA Dryden Flight Research Center from 1946 to 1995

Women in flight research at NASA Dryden ...

Flight tests of external modifications used to reduce blunt base drag

Flight tests of external modifications u...

You Might Also Like

More in Aerodynamics

Aircraft accident report

Aircraft accident report

United States. National Transportation Safety Board.

Aerodynamics for engineering students

Aerodynamics for engineering students

E. L. Houghton

Wind Loading of Structures

Wind Loading of Structures

John D. Holmes

English-Greek dictionary

English-Greek dictionary

S. C. Woodhouse

Fluid-Structure-Sound Interactions and Control

Fluid-Structure-Sound Interactions and C...

Yu Zhou

Flight

Jack Challoner