F-14B :
Fuselage aerodynamics changed
Thrust and torque coefficients at sea level 1400 - 2400 km/h TAS lowered
Afterburner thrust coefficient at sea level 1000 km/h TAS increased
Afterburner thrust coefficient at sea level 1200 - 2400 km/h TAS lowered
Afterburner thrust coefficient at 3 km 1200 km/h TAS increased
Afterburner thrust coefficient at 3 km 1400+ km/h TAS lowered
Afterburner thrust coefficient at 6 km 1000 km/h TAS increased
Afterburner thrust coefficient at 6 km 1400+ km/h TAS lowered
Afterburner thrust coefficient at 9 km 1900 - 2200 km/h TAS increased
Afterburner thrust coefficient at 9 km 2600 km/h TAS lowered
Afterburner thrust coefficient at 12 km 1900 km/h TAS lowered
Afterburner thrust coefficient at 12 km 2200 km/h TAS increased
Afterburner thrust coefficient at 12 km 2600 km/h TAS lowered
Afterburner thrust coefficient at 15 km 2200 km/h TAS increased
Added lead indicator
대충 요약하면...
- 속도대별 추력 변경 (버프도 있고 너프도 있음)
- 레이더 리드 추가
- 동체 공기 역학(?) 변경
속도대별 추력 변경은 주로 고속 영역대에서의 추력 너프인데 아마 공방에서 체감하는 일은 그렇게 많지 않을 것같다는 생각. 동체 공기 역학 변경이 뭔지 궁금해지는데 변경된 후에 테플 돌려봤을 땐 달라진 점 크게 못 느끼긴 했음.
