Aerodynamic characteristics of a hypersonic research airplane concept having a 70 ̊swept double-delta wing at Mach numbers from 0.80 to 1.20, with summary of data from 0.20 to 6.0 View on Open Library

Aerodynamic characteristics of a hypersonic research airplane concept having a 70 ̊swept double-delta wing at Mach numbers from 0.80 to 1.20, with summary of data from 0.20 to 6.0

by Jim A. Penland

No reviews yet
First published: 1979 1 language
Subjects
Aerodynamics Aerodynamic characteristics Computational fluid dynamics Delta wings Hypersonic aircraft Wind tunnel tests

Reviews

Log in or sign up to write a review.

No reviews yet. Be the first!

More by Jim A. Penland

Wall-temperature effects on the aerodynamics of a hydrogen-fueled transport concept in Mach 8 blowdown and shock tunnels

Wall-temperature effects on the aerodyna...

Invariance of hypersonic normal force coefficients with Reynolds number and determination of inviscid wave drag from laminar experimental results

Invariance of hypersonic normal force co...

Effect of Reynolds number variation on aerodynamics of a hydrogen-fueled transport concept at Mach 6

Effect of Reynolds number variation on a...

Aerodynamic characteristics of a distinct wing-body configuration at Mach 6

Aerodynamic characteristics of a distinc...

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

Flight

Jack Challoner