Publication:
Projectile thrust-drag optimization with external burning

Loading...
Thumbnail Image
Authors
Smithey, William John Henry
Subjects
Advisors
Fuhs, Allen E.
Date of Issue
1974-06
Date
Publisher
Monterey, California. Naval Postgraduate School
Language
en_US
Abstract
External burning increases base pressure. The characteristic and linearized equations with heat addition are discuss ed, and the condition for maintaining irrotationa ity with heat addition is derived. A transition model, which extends the Crocco-Lees base flow model, and a spin model are discussed. Computed results are compared with experiment. The optimum location for supersonic external burning is given.
Type
Thesis
Description
Series/Report No
Department
Aeronautics
Organization
Identifiers
NPS Report Number
Sponsors
Funder
Format
Citation
Distribution Statement
Approved for public release; distribution is unlimited.
Rights
This publication is a work of the U.S. Government as defined in Title 17, United States Code, Section 101. Copyright protection is not available for this work in the United States.
Collections