Propulsion/Weapon System Interaction Model
Abstract
This document described a computer program used to evaluate advanced air breathing propulsion payoffs in aircraft performance of future interest to the USAF. The program is required to determine the potential impact of propulsion technology advancements and future weapon system requirements on propulsion concept and cycle selection. A major requirement in such assessments is the evaluation of interaction effects between the engine and airframe. Several scalable airframe Data bases were developed to examine a variety of vehicle concepts including a tactical fighter, supersonic interceptor, supersonic cruise missile, logistic transport, lightweight fighter, carrier air vehicle (first stage of a two-stage-to-orbit system) and hypersonic interceptor. A program description including options, mission analysis approach, installation methodology, and program structure is provided. A description of each of the existing data bases including baseline weights, dimensions, and drag characteristics is included. Also, a sample output listing is included in this document.... Engine/Airframe computer performance model, Propulsion installation, Mission analysis.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jul 01, 1992
- Accession Number
- ADA259291
Entities
People
- Colin Widdison
Organizations
- Boeing Military Aircraft