Extension of the Method for Predicting Six-Degree-of-Freedom Store Separation Trajectories at Speeds up to the Critical Speed to Include a Fuselage with Noncircular Cross Section. Volume I - Theoretical Methods and Comparisons with Experiment

Abstract

The primary objective of this report is to describe improvements and extensions which have been made to the method of predicting six-degree-of-freedom trajectories of stores released from fighter-bomber aircraft previously published by the authors in AFFDL-TR-72-83. In the present work, the circular fuselage restriction has been removed. Methods are presented for flow modeling fuselages with non-circular cross sections including canopies and engine air inlets.

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Document Details

Document Type
Technical Report
Publication Date
Nov 01, 1974
Accession Number
ADA005822

Entities

People

  • Frederick K. Goodwin
  • Jack N. Nielsen
  • Marnix F. E. Dillenius

Organizations

  • Nielsen Engineering & Research (United States)

Tags

DTIC Thesaurus Topics

  • Air Force
  • Aircraft Equipment
  • Aircrafts
  • Computer Programs
  • Computers
  • Contracts
  • Experimental Data
  • Flow Fields
  • Free Stream
  • Fuselages
  • Governments
  • Load Distribution
  • Shape
  • Two Dimensional
  • Wind Tunnel Models
  • Wind Tunnel Tests
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Aerospace Engineering
  • Control Systems Engineering.