Stability and control characteristics of a monoplanar missile configuration with triform-tail-fin arrangements at mach numbers from 1.70 to 2.86 /

Stability and control characteristics of a monoplanar missile configuration with triform-tail-fin arrangements at mach numbers from 1.70 to 2.86 / Milton Lamb.

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Bibliographic Details
Online Access:	Search for the full-text version of this title in HathiTrust
Main Author:	Lamb, Milton
Corporate Authors:	United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, Langley Research Center
Format:	Government Document Book
Language:	English
Published:	Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1981.
Series:	NASA technical memorandum ; 83223.
Subjects:	Guided missiles > Control systems > Testing. Guided missiles > Aerodynamics > Testing. Wind tunnels > Testing.

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Call Number:	NAS 1.15:83223
NAS 1.15:83223	Restricted Place a Hold

Norlin Library - Government Information - US

Holdings details from Norlin Library - Government Information - US
Call Number:	NAS 1.15:83223
NAS 1.15:83223	Available Place a Hold