Accession Number:

ADA446749

Title:

A Hypersonic Vehicle Model Developed with Piston Theory (Preprint)

Descriptive Note:

Conference paper 1 Jan 2005-9 Jan 2006

Corporate Author:

AIR FORCE RESEARCH LAB WRIGHT-PATTERSON AFB OH AIR VEHICLES DIRECTORATE

Report Date:

2006-01-01

Pagination or Media Count:

9.0

Abstract:

For high Mach number flows, M 4, piston theory has been used to calculate the pressures on the surfaces of a vehicle. In a two-dimensional flow, a perpendicular column of fluid stays intact as it passes over a solid surface. Thus, the pressure at the surface can be calculated assuming the surface were a piston moving into a column of fluid. In this work, piston theory is used to calculate the rigid body forces, moments, and stability derivatives of a hypothetical hypersonic vehicle. Only longitudinal motion is considered in this case and lateral motion will be included in subsequent work.

Subject Categories:

  • Research and Experimental Aircraft
  • Reciprocating and Rotating Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE