Scramjet engine 조사
차례 Scramjet 이란? 가스터빈엔진과 구조적 차이점 Ramjet 과의 차이점 scramjet의 구조와 운용범위 내부 초음속연소과정 현재 운용중인 scramjet 비행체 개발중인 scramjet 비행체 reference
What is a scramjet? A scramjet is a kinetic compression(ramjet) with a supersonic air through-flow supersonic combustion ramjet Combustion speed remains 35 μsec ± 5 μsec
가스터빈엔진과 구조적차이점(1)
가스터빈엔진과 구조적차이점(2) ramjet Scramjet
Ramjet 과의 차이점 Ramjet Scramjet
scramjet의 구조와 운용범위(1)
scramjet의 구조와 운용범위(2)
scramjet의 구조와 운용범위(3)
scramjet의 구조와 운용범위(4)
Premixing process
내부초음속연소모습(1) Strong Interaction in CP1 : the growth rate(dc/x) of mixing layer starts to increase significantly after CP1 Weak Interaction in CP2 , CP3: smaller density gradient between fuel and air within the mixing layer CP1 : first crossing point CP2: second crossing point CP3: third crossing point δc : mixing layer thickness
내부초음속연소모습(2)
내부초음속연소모습(3-1)
내부초음속연소모습(3-2) The mixing/combustion efficiency is increased when wedge is positioned adequately.
내부초음속연소모습(4) Supersonic Flame ( Increasing Fuel)
Supersonic Flame ( Increasing Air) 내부초음속연소모습(5) Supersonic Flame ( Increasing Air)
WHY IS IT SO EXPENSIVE?
J-58 Pratt and Whitney Engine 현재 운용중인 turbo-ramjet비행체(1) J-58 Pratt and Whitney Engine SR71
현재 운용중인 turbo- ramjet비행체(2) <<Specifications: >> Model: Pratt & Whitney J-58JT11D-20 Compressor: 9-stage, axial flow, single spool Turbine: two-stage axial flow Thrust: 32,500 lbs. with afterburner Weight: approx. 6,000 lbs. Max. operating altitude: above 80,000 ft.
Closeup of J-58 Inlet with Spike Removed SR71 엔진모습 Closeup of J-58 Inlet with Spike Removed
Scramjet Engine Hyper-X (Future) Mach 10
Reference http://jpl.snu.ac.kr/research/highspeed/supersonic/SupConcept.htm http://www.wvi.com/~lelandh/j-58~1.htm http://www.aviation-history.com/engines/ramjet.htm http://www.physics.uq.edu.au:8001/lp/lasdiag/scram.htm http://www.atse.org.au/publications/focus/focus-stalker.htm http://www.grc.nasa.gov/WWW/K-12/airplane/rampart.htm http://www.hq.nasa.gov/office/pao/History/SP-440/ch8-2.htm