Theorems concerning the reduction of drag for supersonic aircraft

Theorems concerning the reduction of drag for supersonic aircraft

In this report the problem of drag reduction or minimization for aircraft in supersonic flight is investigated within the framework of linearized theory of inviscid flow for fixed flight Mach number. General theorems applicable to complete aircraft configurations are developed. These theorems state...

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Bibliographic Details
Main Author: Rodriguez, Alexander Martin
Format: Others
Published: 1956
Online Access:https://thesis.library.caltech.edu/3282/1/Rodriguez_am_1956.pdf
Rodriguez, Alexander Martin (1956) Theorems concerning the reduction of drag for supersonic aircraft. Dissertation (Ph.D.), California Institute of Technology. doi:10.7907/R1JD-WT10. https://resolver.caltech.edu/CaltechETD:etd-08302006-133358 <https://resolver.caltech.edu/CaltechETD:etd-08302006-133358>

Internet

https://thesis.library.caltech.edu/3282/1/Rodriguez_am_1956.pdf
Rodriguez, Alexander Martin (1956) Theorems concerning the reduction of drag for supersonic aircraft. Dissertation (Ph.D.), California Institute of Technology. doi:10.7907/R1JD-WT10. https://resolver.caltech.edu/CaltechETD:etd-08302006-133358 <https://resolver.caltech.edu/CaltechETD:etd-08302006-133358>

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