Impulse function and drag in scramjet inlet models
- 1 November 1996
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Propulsion and Power
- Vol. 12 (6) , 1181-1183
- https://doi.org/10.2514/3.24161
Abstract
No abstract availableKeywords
This publication has 8 references indexed in Scilit:
- Magnetic flow meter measurement of solid propellant pressure-coupled responses using an acoustic analysisJournal of Propulsion and Power, 1996
- Dynamics of aluminum combustionJournal of Propulsion and Power, 1995
- Hypersonic Airbreathing PropulsionPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1994
- Numerical study of the effects of reverse sweep on scramjet inlet performanceJournal of Propulsion and Power, 1992
- Numerical and experimental investigation of airframe-integrated inlet for high velocitiesJournal of Propulsion and Power, 1992
- Direct measurement of high frequency, solid propellant, pressure-coupled admittancesJournal of Propulsion and Power, 1987
- Linear analysis of forced longitudinal waves in rocket motor chambersAIAA Journal, 1981
- The Stability of One-Dimensional Motions in a Rocket MotorCombustion Science and Technology, 1973