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A study of second-order supersonic-flow theory

Van Dyke, Milton D. (1951) A study of second-order supersonic-flow theory. NACA Technical Notes, 2200. National Advisory Committee for Aeronautics , Washington, DC. (Submitted) http://resolver.caltech.edu/CaltechAUTHORS:20171101-110011445

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Abstract

Second-order solutions of supersonic-flow problems are sought by iteration, using the linearized solution as the first step. For plane and axially symmetric flows, particular solutions of the iteration equation are discovered which reduce the second-order problem to an equivalent linearized problem. Comparison of second-order solutions with exact and numerical results shows great improvement over linearized theory. For full three-dimensional flow, only a partial particular solution is found. The inclined cone is solved, and the possibility of treating more general problems is considered.


Item Type:Report or Paper (Technical Report)
Related URLs:
URLURL TypeDescription
http://www.technicalreports.org/trail/detail/44192/OrganizationTechnical Report
http://resolver.caltech.edu/CaltechTHESIS:12062017-085319714Related ItemThesis
Group:GALCIT
Subject Keywords:Fundamental aerodynamics; Supersonic flow; Bodies - Aerodynamic theory
Other Numbering System:
Other Numbering System NameOther Numbering System ID
GALCIT Publication266
Record Number:CaltechAUTHORS:20171101-110011445
Persistent URL:http://resolver.caltech.edu/CaltechAUTHORS:20171101-110011445
Usage Policy:No commercial reproduction, distribution, display or performance rights in this work are provided.
ID Code:82829
Collection:CaltechAUTHORS
Deposited By: Melissa Ray
Deposited On:03 Nov 2017 17:20
Last Modified:06 Dec 2017 17:01

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