NDLI: Aerodynamic characteristics of a series of airbreathing missile configurations

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Aerodynamic characteristics of a series of airbreathing missile configurations

Content Provider	NASA Technical Reports Server (NTRS)
Author	Hayes, C.
Copyright Year	1981
Description	Due to the interest in the application of airbreathing propulsion to missiles and the lack of a suitable data base, an experimental program has been conducted to contribute to such a data base. The configurations investigated were with twin-inlets, either two-dimensional or axisymmetric, each located at three circumferential locations. The effects of a wing located above the inlets and of tail configuration were investigated. Longitudinal stability and control and lateral-directional stability were included in the data obtained. This paper presents a summary of the program and some of the results obtained. Certain trends of the data, as well as problem areas, are discussed. Due to the large volume of data obtained, a detailed analysis is not presented.
File Size	325201
Page Count	9
File Format	PDF
Alternate Webpage(s)	http://archive.org/details/NASA_NTRS_Archive_19820018479
Archival Resource Key	ark:/13960/t05x74s9m
Language	English
Publisher Date	1981-05-14
Access Restriction	Open
Subject Keyword	Launch Vehicles And Space Vehicles Missile Configurations Pitching Moments Directional Stability Aerodynamic Configurations Body-wing and Tail Configurations Lateral Stability Inlet Nozzles Air Breathing Engines Control Stability Aerodynamic Characteristics Propulsion System Configurations Tail Surfaces Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science
Content Type	Text
Resource Type	Technical Report

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