Accession Number : ADA320802

Title :   Nonlinear Interaction Between Acoustics and Propellant Combustion.

Descriptive Note : Final rept.,

Corporate Author : UNIVERSITA DEGLI STUDI DI TORINO (ITALY) DIPT DI INGEGNERIA AEROSPAZIALE

Personal Author(s) : Novozhilov, Boris V.

PDF Url : ADA320802

Report Date : DEC 1996

Pagination or Media Count : 36

Abstract : This report results from a contract tasking Dipanmento Di Ingegneria Aerospaziale as follows: The contractor will review Russian works on response function of solid propellant combustion to oscillatory pressure and on acoustic admittance. Differences and similarities between US and Russian approaches to this problem shall be considered.

Descriptors :   *BURNING RATE, *SOLID ROCKET PROPELLANTS, PRESSURE GRADIENTS, MATHEMATICAL MODELS, THERMAL DIFFUSION, PARTIAL DIFFERENTIAL EQUATIONS, ITALY, RUSSIA, UNSTEADY FLOW, FLAME PROPAGATION, COMBUSTION STABILITY, INTEGRAL EQUATIONS, ACOUSTIC PROPERTIES, PROPELLANT BURN OUT, UNITED KINGDOM.

Subject Categories : Combustion and Ignition
      Solid Rocket Propellants

Distribution Statement : APPROVED FOR PUBLIC RELEASE