A Numerical Method for the Calculation of the Inertial Loads on an Airplane Page: III
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TABL>i OF CONTENTS
Page
ii
I NTR ODU CTI0 i I iii
Chapter
I. DEx"1! Ill TI0 N OF y A JIG TEi-1113. . 1
II. STATSitSHT OF BASIC ASSUMPTIONS 3
III. oASIC C ONCEPTS 7
Matrix-Vector Notation
Integration of a Matrix
IV. DISTRIBUTION .STATIONS . . . 9
General
Fuselage
Horizontal Surfaces
Vertical Surfaces
V. CALCULATION OF INSRTIA CHARACTERISTICS 27
General
Intervals of a Component
Complete Component
Complete Airplane
VI. CALCULATION OF UNIT INSRTIAL LOADS
ON AN AIRPL \NE.
Inertial Loads Within a Rigid Sody
Formulation of the Matrix of "Unit Inertial Loads
Transfer of the Unit Inertial Loads
of an Attached Component into
the Unit Inertial Loads of the
Parent Component
BI3LI0GRAPIIY i|9
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Williams, Glen R. A Numerical Method for the Calculation of the Inertial Loads on an Airplane, thesis, January 1958; Denton, Texas. (https://digital.library.unt.edu/ark:/67531/metadc107988/m1/3/?rotate=270: accessed July 18, 2024), University of North Texas Libraries, UNT Digital Library, https://digital.library.unt.edu; .