Back to results
Virginia Tech
The prediction of aerodynamic force and moment coefficients on elliptic cone bodies at both angle of attack and sideslip by use of Newtonian impact theory
Abstract
dc:description.abstractNewtonian theory was applied, in this analysis, to the elliptic cone segment at angles of attack and sideslip. Closed form expressions for the aerodynamic coefficients and static stability derivatives were obtained. Expressions for the full and half conic bodies were given and approximate expressions were given for the half cone case. The circular cone results were obtained as a special case of the general results. Comparisons of the theoretical calculations with experimental results at hypersonic speeds were made of the aerodynamic coefficients and static derivatives for several conic segments. Generally, good agreement was observed for specified ranges of fineness ratios and angles of attack.
Degree
thesis:*- Name thesis:degree_name
- Master of Science
- Level thesis:degree_level
- masters
- Discipline thesis:degree_discipline
- Aeronautical Engineering
- Department dc:contributor.department
- Aeronautical Engineering
- Grantor dc:publisher
- Virginia Tech
- Year dc:date.issued
- 1961
Author and committee
dc:creator, dc:contributor.*- Author dc:creator
-
- Wells, William R.
- Chair dc:contributor.committeechair
-
- Hassan, Hassan A.
- Committee member dc:contributor.committeemember
-
- Truitt, Robert W.
Rights
dc:rights- Statement dc:rights
-
- In Copyright
- Licence dc:rights.uri
- Language dc:language.iso
- en
Identifiers
dc:identifier.*- Dc Identifier Other
- etd-09082012-040433
- OAI identifier oai:identifier
- oai:vtechworks.lib.vt.edu:10919/44672