An investigation of the aerodynamic effects of a two-radome installation on a Challenger aircraft.

It appears your Web browser is not configured to display PDF files. Download adobe Acrobat or click here to download the PDF file.

Click here to download the PDF file.

Creator: 

Chinoy, Zubin

Date: 

1998

Subject: 

Radomes -- Mathematical Models
Boundary Layer
Drag (Aerodynamics)
Reynolds Number
Wind Tunnel Models

Language: 

English

Publisher: 

Carleton University

Identifier: 

Proquest Record
Library Catalogue Record
https://doi.org/10.22215/etd/1998-03920

Thesis Degree Name: 

Master of Engineering: 
M.Eng.

Thesis Degree Level: 

Master's

Thesis Degree Discipline: 

Engineering, Mechanical and Aerospace

Parent Collection: 

Theses and Dissertations

Items in CURVE are protected by copyright, with all rights reserved, unless otherwise indicated. They are made available with permission from the author(s).