NONLINEAR COMBUSTION INSTABILITY IN A SOLID PROPELLANT TWO-DIMENSIONAL WINDOW MOTOR

Authors
  1. Hughes, P.M.
  2. Saber, A.J.
Corporate Authors
Defence Research Establishment Valcartier, Valcartier QUE (CAN);American Inst of Aeronautics and Astronautics, New York NY (US)
Abstract
Shock wave, or nonlinear instability typically found in solid propellant rocket motors with high L/D ratios is discussed. Schlieren-streak photography and chamber pressure measurements taken from a two-dimensional windowed rocket motor are reported. In an analytical model the passage of an incident shock through the combustion products is examined.
Report Number
PAPER-78-1008 — Reprint 4213
Date of publication
01 Jan 1978
Number of Pages
6
Reprinted from
AIAA/SAE 14th Joint Propulsion Conference, Las Vegas, Nev, July 25-27, 1978
DSTKIM No
78-02856
CANDIS No
83540
Format(s):
Hardcopy;Originator's fiche received by DSIS

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