SUPERSONIC FLUTTER OF MISSILES WITH FLEXIBLE BODIES

Abstract

AD-265 8799N2 AD-265 880Div. 9, 12U (TIPTW/WAW) OTS price $1.10 Midwest Research Inst., Kansas City, Mo. SUPERSONIC FLUTTER OF MISSILES WITH FLEXIBLE BODIES. Bimonthly progress rept. no. 1, 8 Apr-8 June 60, by Edmond F. E. Zeijdel. 11 July 60, 3p. (Contract NOw 60-0726-c; Continuation of Contract NOa(s) 59-6135-c) Unclassified report DESCRIPTORS: (*Guided missiles, *F LUTTER, Mathematical analysis, Differential equations, Partial differential equations, *Supersonics, Aerodynamics, Wings.) The primary objective of this research program is to determine the unsteady aerodynamic forces on slender supersonic missiles. The unsteady aerodynamic forces will be determined on the basis of quasi-slender body theory and particular emphasis will be placed on the case of wing bending. This work is a continuation of work completed under BuAer Contract NOas 59-6135-c (AD-242 907). During this report period, initial efforts were made to give an example which illustrates the theory developed under the previous contract. (Author)

Document Details

Document Type
Technical Report
Publication Date
Aug 16, 1960
Accession Number
AD0265879

Entities

People

  • Edmond F.e. Zeijdel

Organizations

  • MRIGlobal

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Aerodynamic Forces
  • Bodies
  • Complex Variables
  • Contracts
  • Differential Equations
  • Equations
  • Guided Missiles
  • Mathematical Analysis
  • Numerical Analysis
  • Partial Differential Equations
  • Slender Bodies
  • Theorems

Readers

  • Aerodynamics/Aeronautics.
  • Calculus or Mathematical Analysis
  • Snow Cover Descriptors for Reptiles and Their Illustrations.

Technology Areas

  • Hypersonics