An Automated Procedure for Flutter and Strength Analysis and Optimization of Aerospace Vehicles. Volume 2. Program User's Manual
Abstract
This volume contains the detailed instructions needed to use the Flutter And STrength Optimization Program (FASTOP). The program is capable of both integrated analysis and efficient (near-minimum weight) sizing of cantilever and free-free lifting surface structures in the presence of strength and flutter-speed constraints. FASTOP consists of two major sub-programs, namely the Structural Optimization Program (SOP), and the Flutter Optimization Program (FOP). The volume contains the following four parts: FASTOP overview, usage/input/output for structural optimization program, usage/input/output for flutter optimization program, and program execution.
Document Details
- Document Type
- Technical Report
- Publication Date
- Dec 01, 1975
- Accession Number
- ADB009781
Entities
People
- Dino George
- George Schriro
- Joel Markowitz
- Keith Wilkinson
- Richard Chipman
Organizations
- Grumman