# 2.33.0.48 -> 2.33.0.50
* New Language : Vietnamese
# 2.33.0.50 -> 2.33.0.52
* Client Stability Improved
# 2.33.0.52 -> 2.33.0.53
* F-111A :
* Wing at 0% sweep
* Oswald’s efficiency number reduced from 0.78 to 0.62
* This will mean a higher coefficient of drag depending on AoA, reducing overall turn
* Lift coefficient after critical AoA reduced from 1.2 to 1.05
* Reduced lift after stall
* Coefficient of drag Mach multiplier curve Critical Mach number from 0.78 to 0.74
* Multiplier will begin applying from M0.74, resulting in slightly increased drag
* Auxiliary Mach multiplier curve multiplier maximum reduced from 1.15 to 1.05
* Slightly reduced coefficient of lift from M0.3 to M0.6
* Induced drag Mach multiplier curve critical Mach number from 0.78 to 0.45
* Induced drag multiplier will begin applying from M0.45 instead of M0.78, resulting in increased induced drag
* Coefficient of lift at critical AoA reduced from 1.52 to 1.42
* Reduced lift at critical AoA
* Wing at 0% sweep, flaps out
* Oswald’s efficiency number reduced from 0.78 to 0.62
* This will mean a higher coefficient of drag depending on AoA, reducing overall turn
* Auxiliary Mach multiplier curve multiplier maximum reduced from 1.15 to 1.05
* Slightly reduced coefficient of lift from M0.3 to M0.6
* Induced drag Mach multiplier curve critical Mach number from 0.78 to 0.45
* Induced drag multiplier will begin applying from M0.45 instead of M0.78, resulting in increased induced drag at lower speeds than before
* Wing at 50% sweep
* Oswald’s efficiency number reduced from 0.71 to 0.54
* This will mean a higher coefficient of drag depending on AoA, reducing overall turn
* Lift coefficient after critical AoA increased from 0.8 to 0.95
* Increased lift after stall
* Induced drag Mach multiplier curve adjustments
* * * * Critical Mach number from 0.78 to 0.5
* Coefficient max value from 1.05 to 1.1
* Induced drag multiplier will begin applying from M0.5 instead of M0.78 and overall have slightly more induced drag both at lower speeds and overall
* Zero-lift drag coefficient increased from 0.0073 to 0.0079
* More overall drag
* Wing at 50% sweep, flaps out
* Oswald’s efficiency number reduced from 0.7 to 0.54
* This will mean a higher coefficient of drag depending on AoA, reducing overall turn
* Lift coefficient after critical AoA decreased from 1.35 to 1.05
* Reduced lift after stall
* Induced drag Mach multiplier curve adjustments
* Critical Mach number from 0.78 to 0.5
* Coefficient max value from 1.05 to 1.1
* Induced drag multiplier will begin applying from M0.5 instead of M0.78 and overall have slightly more induced drag both at lower speeds and overall
* Wing at 100% sweep
* Oswald’s efficiency number reduced from 0.61 to 0.5
* This will mean a higher coefficient of drag depending on AoA, reducing overall turn
* Induced drag Mach multiplier curve adjustments
* Critical Mach number from 0.78 to 0.5
* Coefficient max value from 1.05 to 1.1
* Induced drag multiplier will begin applying from M0.5 instead of M0.78 and overall have slightly more induced drag both at lower speeds and overall
* Lift coefficient at critical AoA adjustments
* High: 1.15 to 1.05
* Low: -1.05 to -0.95
* Slightly less lift at critical AoA, slightly more at negative critical AoA
* Zero-lift drag coefficient reduced from 0.008 to 0.0077
* Less overall drag
* Wing at 100% sweep, flaps out
* Oswald’s efficiency number reduced from 0.61 to 0.5
* This will mean a higher coefficient of drag depending on AoA, reducing overall turn
* Induced drag Mach multiplier curve adjustments
* * * * Critical Mach number from 0.78 to 0.5
* Coefficient max value from 1.05 to 1.1
* Induced drag multiplier will begin applying from M0.5 instead of M0.78 and overall have slightly more induced drag both at lower speeds and overall
* Thrust maximum number before calculation reduced from 4940 to 4400 kgf
* After calculation, this will express in a loss of around 1000-3000 kgf overall at any speed
* IL-2M (1943) : Enabled canopy control
* JAS39A, JAS39C :
* Wing
* Oswald’s efficiency number increased from 0.52 to 0.53
* This will mean a very slightly lower coefficient of drag depending on AoA, increasing overall turn
* Coefficient of drag Mach multiplier curve adjustments
* Critical Mach number from 0.9 to 0.92
* Coefficient max value from 1.6 to 1.55
* Multiplier will begin applying a tad bit later at M0.92 and overall have a bit less drag from M0.92 to M1.03 than previously
* Induced drag Mach multiplier curve adjustments
* Critical Mach number from 0.3 to 0.25
* Coefficient max value from 0.88 to 0.78
* Multiplier will begin applying from M0.25 instead of M0.3 and overall will have slightly more induced drag from M0.25 to M0.6
* Zero-lift drag coefficient reduction from 0.008 to 0.0068
* Overall less drag
* Wing with flaps out
* Oswald’s efficiency number increased from 0.52 to 0.53
* This will mean a very slightly lower coefficient of drag depending on AoA, increasing overall turn
* Coefficient of drag Mach multiplier curve adjustments
* Critical Mach number from 0.9 to 0.92
* Coefficient max value from 1.6 to 1.55
* Multiplier will begin applying a tad bit later at M0.92 and overall have a bit less drag from M0.92 to M1.03 than previously
* Induced drag Mach multiplier curve adjustments
* Critical Mach number from 0.3 to 0.25
* Coefficient max value from 0.88 to 0.78
* * * * Multiplier will begin applying from M0.25 instead of M0.3 and overall will have slightly more induced drag from M0.25 to M0.6
* Zero-lift drag coefficient reduction from 0.021 to 0.018
* Overall less drag
* Fuselage
* Coefficient of drag Mach multiplier curve coefficient max from 2.45 to 2.25
* Lower drag multiplier from M0.92 to M1.05
* Zero-lift drag coefficient reduction from 0.0061 to 0.0044
* Overall less drag
* Very slightly increased elevator deflection at 2000 m from 1000-1900 km/h TAS
* Peak thrust changes
* Thrust maximum number before calculation increased from 5100 to 5340 kgf
* Only really matters for really really high altitudes because most of the thrust curve has been adjusted
* At 0 m, 0-2000 km/h TAS
* At 0 km/h from 7500 kgf to 8080 kgf
* At 250 km/h from 7320 kgf to 8040 kgf
* At 500 km/h from 7780 kgf to 8200 kgf
* At 750 km/h from 8950 kgf to 8840 kgf
* At 1000 km/h from 10125 kgf to 9140 kgf
* At 1250 km/h from 10900 kgf to 8940 kgf
* At 1500 km/h from 10800 kgf to 8050 kgf
* At 1750 km/h from 9800 kgf to 8070 kgf
* At 2000 km/h from 9030 kgf to 8090 kgf
* At 3000 m, 250-2000 km/h TAS
* At 250 km/h from 6370 kgf to 6700 kgf
* At 500 km/h from 6580 kgf to 6880 kgf
* At 750 km/h from 7250 kgf to 7100 kgf
* At 1000 km/h from 8110 kgf to 7820 kgf
* At 1250 km/h from 8900 kgf to 8840 kgf
* At 1500 km/h from 9500 kgf to 8830 kgf
* At 1750 km/h from 9600 kgf to 8700 kgf
* At 2000 km/h from 9250 kgf to 8550 kgf
* * * At 6000 m, 250-2000 km/h TAS
* At 250 km/h from 5160 kgf to 5350 kgf
* At 500 km/h from 5550 kgf to 5500 kgf
* At 750 km/h from 6060 kgf to 5860 kgf
* At 1000 km/h from 6550 kgf to 6300 kgf
* At 1250 km/h from 7200 kgf to 6830 kgf
* At 1500 km/h from 7680 kgf to 7500 kgf
* At 1750 km/h from 8080 kgf to 8400 kgf
* At 2000 km/h from 7950 kgf to 8970 kgf
* At 9000 m, 0-2000 km/h TAS
* At 0 km/h from 3760 kgf to 3950 kgf
* At 250 km/h from 3910 kgf to 3900 kgf
* At 500 km/h from 4220 kgf to 4090 kgf
* At 750 km/h from 4550 kgf to 4310 kgf
* At 1000 km/h from 4930 kgf to 4750 kgf
* At 1250 km/h from 5500 kgf to 5320 kgf
* At 1500 km/h from 5880 kgf to 5750 kgf
* At 1750 km/h from 6080 kgf to 6000 kgf
* At 2000 km/h from 6080 kgf to 6130 kgf
* At 12000 m, 0-2000 km/h TAS
* At 0 km/h from 2400 kgf to 2180 kgf
* At 250 km/h from 2560 kgf to 2140 kgf
* At 500 km/h from 2870 kgf to 2200 kgf
* At 750 km/h from 3200 kgf to 2360 kgf
* At 1000 km/h from 3610 kgf to 2840 kgf
* At 1250 km/h from 4000 kgf to 3500 kgf
* At 1500 km/h from 4280 kgf to 4340 kgf
* At 1750 km/h from 4430 kgf to 4980 kgf
* At 2000 km/h from 4520 kgf to 5270 kgf
* Enabled center gear braking
* Autopilot max overload rate adjustment
* From [-5, 13] to [-5, 16]
* Will reach peak G slightly slower in a pull
# 2.33.0.53 -> 2.33.0.54
* Vilkas :
* Armor Rework
* Spike-LR2MR ATGM : Ammo Count : 2 -> 4
* New Texts :
* "Severe Damaged"
Current Dev version : 2.33.0.54
Current Live version : 2.33.0.52
구독자 7959명
알림수신 127명
워썬더, 인리스티드 등 가이진 퍼블리싱 게임 채널
워썬더 소식
2.33.0.54 F111&그리펜,[빌카스 버프]
추천
5
비추천
0
댓글
15
조회수
1594
작성일
댓글
[15]
군소
순순히애를낳아
POLTAVA
LITTORIO
POLTAVA
zlong
대영제국
ㅇㅇ
카나타의남편
수27노즐에질내사정
ㅇㅇ
더블배럴
LITTORIO
IlIllIlllllIIIIl
M3전차
본 게시물에 댓글을 작성하실 권한이 없습니다.
로그인 하신 후 댓글을 다실 수 있습니다. 아카라이브 로그인
최근
최근 방문 채널
최근 방문 채널
번호
제목
작성일
조회수
추천
공지
아카라이브 모바일 앱 이용 안내(iOS/Android)
28460435
공지
[eSport] Air Superiority 2024를 관람하시고, 특별한 Twitch Drops 를 획득하세요!
1964
공지
가이진채널 통합공지
11620
공지
가이진채널 규정&신문고
7097
공지
채널 홍보용 글
410069
공지
아무도 관심 없을 내용
18533
공지
당신도 할 수 있다! 남녀노소 누구나 가능한 버그 제보
8098
공지
다시 돌아온 가챈 설문조사 - Alpha Strike 지상전 설문결과
1830
공지
다시 돌아온 가챈 설문조사 - Alpha Strike 공중전 설문결과
2126
숨겨진 공지 펼치기(4개)
악마의 살인달구지
[4]
116
1
니니 니자로 시작하는말은~
[12]
259
3
이거 존나 웃기네 ㅋㅋ
[8]
182
1
시발 프랑스 타는놈들은 저랭 어케뚫은거임
[62]
404
3
탑젯 응우옌맵 좆같네
[1]
60
0
하 이걸 안사네
[3]
148
0
폭격감자는 ㄹㅇ못타먹겠음
[3]
114
0
성탄절 도색 ㅆㅌㅊ
[5]
194
6
아드바크 오스왈드 떡너프 뭐노
[4]
426
2
저런 저속 추력 있으면 퇴근시간 몇시냐?
[10]
210
0
✋질문
할인 기간에 5만원 지를건데
[7]
249
0
항력버프에 추력너프면 무슨차이점이 생기지
[5]
302
0
폭격감자이거 기동 ㅎㅌㅊ인가 s텀한테도 뒤를잡히네
[12]
263
2
븜프 너가 그렇게 곡사를 잘해?
110
0
그리펜 바뀐 추력특성 ㄹㅇ 호넷 따라가는거같은데
269
0
2S35는 열상레거측스테빌 있나
[6]
150
0
그리펜 추력 떡너프당했네
[6]
451
6
빌카스 제발 병신이어라 기도중인 새끼
[9]
340
0
2023브븜
[1]
211
0
K9 99식 있는데 이겄도 넣어줘
[14]
367
2
그리펜 씨발 진짜 또 버프야
[6]
322
0
그리펜 저속기동 버프네
112
0
비다르 뭔 씨발 ㅋㅋㅋㅋ
[8]
399
2
워썬더 소식
2.33.0.54 F111&그리펜,[빌카스 버프]
[15]
1595
5
'그거' 오냐
[6]
179
0
적군 응디에 쏜 미사일이
[1]
102
0
킬로그이거 ㅈㄴ웃기네 ㅋㅋㅋㅋㅋ
167
0
전부 골장비타러들갔나
[2]
190
0
생각보다 미베런 별로 없네
[5]
142
0
7.7덱 만든다고 프랑스만 타는데 4초 맛보니 딴거못타겠네
[8]
178
0
23믈이 11.3 최강이라고?
[26]
407
0
이건 또 뭔 병신버그래
[3]
152
0
핀라켄 재밌네
[2]
138
0
아니시발 비행기좀더워서 구멍하나뚫었는데 기름이 줄줄새네
[3]
242
1
가붕이 현 좆백수 사
[13]
242
0
허접ㅋㅋㅋㅋㅋ
[1]
85
1
자탑 23믈은 신인데?
[3]
235
0
세일 이틀차아닌가 로캣런뛰는애들은없고 탑젯만걸리네
133
0
시발 존나 지능적으로겜하네
[3]
172
1
피자는 좀 빠져있어~
113
0
독장연 지금 탑지상만 ㅈㄴ잘하는게 아닌거같은데
[4]
217
0
우흥~ 우흥~
69
0
지상전 못하겠다.
[5]
166
1
이벤트로 8랭 제트기 건즈온리 모드 나오면 좋겠다
[8]
255
7
근데 뱅리얼이거 로캣런이랑 공중전이랑 보상차이너무나는거아니냐
[5]
154
0