@Ultra_Tom 나이 어린것 자체는 경쟁력이 될 수가 있지요. 원하는 ‘경력(현 메타에 맞는)’ 을 갖추면서 핸들링 쉽다면 그것만으로도 경쟁력이 있죠.
세대 간 경쟁이라는건 님이 하신 그 말씀에 잘 나와있네요. 20대에 데여 적대하고싶다는 생각은 잘 알겠습니다만, 그러고서 ‘세대간 경쟁이라는 관점~ (계속)
대규모 정리해고? 익명 커뮤니티 ‘블라인드’는 석달 먼저 안다 https://t.co/Q0GUberoWQ
“예전에는 회사에서 잘려도 갈 곳이 있었지만, 요즘은 일자리 찾기가 점점 어려워져 고용의 유연성이 높은 미국에서도 심리적 충격이 크다”
“한국에선 중간 단계 없이 곧바로 전 직군 해고로 이어질 수 있다.”
@Ultra_Tom 그거 일반 기술 분야에도 적용되는 이야기인데요?
최신 기술 발전이 세대를 거듭하며 발전된 건 부정되진 않지만 그 중간에 발전 못 따라가서 도태되는 사람들은 언제나 있어왔구요.
최신 기술 습득도 머리가‘말랑말랑할’ 때 수월하지 자기 일하는 방식 굳어진 다음엔 힘들어지지요.
UEC R&D work on variable cycle/variable bypass engines ( Product 30 as base )
Scientific and Technical Challenges:
1 > Selection of the air extraction point from the low-pressure compressor (LPC).
2 > Selection of the air injection point for the third bypass stream (third contour) into the engine flow path.
3 >Integration of the third contour with the aircraft engine nacelle.
4 > Resolution of testing issues for the engine with the third contour under flight conditions (test stand modernization).
5> Components of the third-contour duct manufactured using additive manufacturing (3D-printing) technologies.
Dimensions Shown
Length: 2283 mm
Diameter: 1560 mm
This diagram appears to describe a Russian turbofan engine concept with a third bypass stream (third contour), related to advanced fuel-efficiency improvements being studied for future aircraft engines.
The table indicates a 3–9% reduction in specific fuel consumption depending on flight conditions.
Credit: @GeorgeN28581
UEC R&D work on variable cycle/variable bypass engines ( Product 30 as base )
Scientific and Technical Challenges:
1 > Selection of the air extraction point from the low-pressure compressor (LPC).
2 > Selection of the air injection point for the third bypass stream (third contour) into the engine flow path.
3 >Integration of the third contour with the aircraft engine nacelle.
4 > Resolution of testing issues for the engine with the third contour under flight conditions (test stand modernization).
5> Components of the third-contour duct manufactured using additive manufacturing (3D-printing) technologies.
Dimensions Shown
Length: 2283 mm
Diameter: 1560 mm
This diagram appears to describe a Russian turbofan engine concept with a third bypass stream (third contour), related to advanced fuel-efficiency improvements being studied for future aircraft engines.
The table indicates a 3–9% reduction in specific fuel consumption depending on flight conditions.
Credit: @GeorgeN28581