NDLI: Response of radiation driven transient burning of AP and HMX using flame modeling

Content Provider	Springer Nature Link
Author	Lee, Changjin Lee, Jae Woo
Copyright Year	2001
Abstract	The radiation driven response function (R $_{q}$) for AP and HMX propellant was obtained and compared with experimental results by using a simple αβγ flame model rather than with detailed chemistry. For an AP propellant, the profile of heat release was assumed by the experimental data. The calculatedR $_{q}$ shows a frequency shift of the peak amplitude to the higher frequency and a decrease in the maximum amplitude as radiation increases. In addition, it was found the increase in the total flux could enhance the mean burning rate $$\bar r_b $$ while the phase differences between the radiation and resulting conduction could consequently reduce the fluctuation amplitude Δy $_{b}$. Fortunately, this is the qualitative duplication of the behavior recently observed in the experiments of RDX propellants. For HMX, the response functionR $_{q}$ has been calculated and showed a quite good agreement with the experimental data. Even though the fairly good agreement ofR $_{q}$ with experimental ones, the unsteady behavior of HMX was not reproduced as the radiation input increased. This is due to lack of the material properties of HMX or the physical understanding of HMX burning at high pressure.
Starting Page	1181
Ending Page	1187
Page Count	7
File Format	PDF
ISSN	1738494X
Journal	Journal of Mechanical Science and Technology
Volume Number	15
Issue Number	8
Language	English
Publisher	Korean Society of Mechanical Engineers
Publisher Date	2001-01-01
Publisher Place	Seoul
Access Restriction	One Nation One Subscription (ONOS)
Subject Keyword	Radiation Response Function Solid Propellant Mechanical Engineering Vibration, Dynamical Systems, Control Industrial and Production Engineering
Content Type	Text
Resource Type	Article
Subject	Mechanics of Materials Mechanical Engineering

Sl.	Authority	Responsibilities	Communication Details
1	Ministry of Education (GoI), Department of Higher Education	Sanctioning Authority	https://www.education.gov.in/ict-initiatives
2	Indian Institute of Technology Kharagpur	Host Institute of the Project: The host institute of the project is responsible for providing infrastructure support and hosting the project	https://www.iitkgp.ac.in
3	National Digital Library of India Office, Indian Institute of Technology Kharagpur	The administrative and infrastructural headquarters of the project	Dr. B. Sutradhar bsutra@ndl.gov.in
4	Project PI / Joint PI	Principal Investigator and Joint Principal Investigators of the project	Dr. B. Sutradhar bsutra@ndl.gov.in Prof. Saswat Chakrabarti will be added soon
5	Website/Portal (Helpdesk)	Queries regarding NDLI and its services	support@ndl.gov.in
6	Contents and Copyright Issues	Queries related to content curation and copyright issues	content@ndl.gov.in
7	National Digital Library of India Club (NDLI Club)	Queries related to NDLI Club formation, support, user awareness program, seminar/symposium, collaboration, social media, promotion, and outreach	clubsupport@ndl.gov.in
8	Digital Preservation Centre (DPC)	Assistance with digitizing and archiving copyright-free printed books	dpc@ndl.gov.in
9	IDR Setup or Support	Queries related to establishment and support of Institutional Digital Repository (IDR) and IDR workshops	idr@ndl.gov.in

Measurement of solid propellant burning rates by analysis of ultrasonic full waveforms

Friction-induced ignition modeling of energetic materials

A burning velocity correlation for premixed hydrogen/air/steam flames

Numerical study of gas-solid reactive flow in a cylinder

Simplified Modeling of Deflagration in Vessels

Nonlinear acoustic-pressure responses of oxygen droplet flames burning in gaseous hydrogen

Combustion and radiation characteristics of oxygen-enhanced inverse diffusion flame

Measurement of burning velocity for bare strand casted with a frozen mixture of nano/micro-aluminum particles and water

Dynamics modeling and modal experimental study of high speed motorized spindle

Response of radiation driven transient burning of AP and HMX using flame modeling

Similar Documents

Measurement of solid propellant burning rates by analysis of ultrasonic full waveforms

Friction-induced ignition modeling of energetic materials

A burning velocity correlation for premixed hydrogen/air/steam flames

Numerical study of gas-solid reactive flow in a cylinder

Simplified Modeling of Deflagration in Vessels

Nonlinear acoustic-pressure responses of oxygen droplet flames burning in gaseous hydrogen

Combustion and radiation characteristics of oxygen-enhanced inverse diffusion flame

Measurement of burning velocity for bare strand casted with a frozen mixture of nano/micro-aluminum particles and water

Dynamics modeling and modal experimental study of high speed motorized spindle

Response of radiation driven transient burning of AP and HMX using flame modeling