Ювиги (земляк),
Звук был понижен нарочно - так вроде было во время войны. Такой ответ нашел где-то от мододелов.
Я поискал по сети инфо для флайт-модел в т.н. expert mod.
Воть что нашел:
"Aachens Flight Models
A little Background:-
Aachen is a professional Aircraft design engineer, we were not sure if we wanted to go in this direction at first, but were so impressed by how much closer to what we have read flying some of these aircraft and fighting in them has come, that it was inconceivable to go back.
We hope that you share the views of the many 'test-pilots'. You retain a choice still anyhow. Using the full work is strictly optional.
Note:- In Stock Configuration Oleg's Flyables are all Stock (by Oleg or TD) although all new aircraft * that Aachen has worked on have his FM's also.
In 'Expert Mode' All of the aircraft below use Aachens FM's. We have altered the Netcode and the encryption for this mode, so that players cannot use the modified ‘Stock’ FM’s on stock servers.
Those that play online require very reasonably that everybody is playing with the same. Expert mode is to protect this desire. List of modified aircrafts
The complete list of planes modified is as follows: Bf109: E1, E1B, E3, E3b, E4, E4B, E4N, E7, E7N, E7NZ F2, F2B, F2trop, F4, F4B, F4trop, F4Z G1, G2, G2trop, G3, G4, G4trop, G5, G6early, G6Erla, G6Late, G6Mid, G6trop, G10, G10C3, G10Erla, G14, G14early, G14AS K4, K4C3, K6, K14
Fw190: A1, A2, A3, A4, A5, A5-165, A7, A7sturm, A8, A9 F8 D9, D9late, D11, D13
G55: G55, G55late, G55-ss0, G55-ss0late
MC: MC200, MC202, MC205, MC205V
P51: P51B, P51C, P51CM, P51D20, P51D20NT, P51D25, P51D30
P40: P40B, P40C, P40E, P40E-M-105, P40M
P38: P38J, P38J10LO, P38J15LO, P38J25LO P38L, P38L5LO, P38Llate
P47: P47D10, P47D22, P47D27, P47D27late
Foreword The modifications of flight and engine models presented in this work have started with an analytical evaluation of aircraft performances. In the following paragraphs a short description of the methodologies adopted in the analytical study can be found, specifically for the evaluation of aircraft polars. Wing and tail polar Are computed by adopting lift line theory (Weiselberger) using non linear section lift data (J.C. Sivells, R.H. Neely). Compressibility effects are taken into account. Normally, lift distribution, finite wing Cy and Cx computed are in very good agreement with computations performed according to DATCOM method (ref. E. Torenbeek, Synthesis of subsonic airplane design). This is due to the fact that studied aircraft configurations are un-swept and have high aspect ratios."
Далее следуют графики и формулы.
По поводу он-лайн - я посетил несколько серваков. К сожалению expert mode включен на 2-3 малопосещаемых серваков.
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