[Vasya]

Мотор для Д-1.

[V-1710-35W-45_9/RIGHT/NEW/P-39D-1]
// Airplane equipped with Allison V-1710-35 engine and a three-bladed Curtiss Electric constant speed propeller,
// blade design No. 614-10-1-5-21, blade angle range 21.5° tp 51.5° at 42 inch radius.
  Direction Right
  HorsePowers 1160.0
  BoostFactor 1.0
  WEPBoostFactor 1.156522
  cAfterburner 1
  AfterburnerType 11  
  cMix 1
  RPMMin 200
  RPMNom 3000.0
  RPMMax 3000.0
  RPMMaxAllowed 3320
  Reductor 0.7336                         // 0.555556
  PropDiameter 3.162                      // 3.162 
  PropMass 166.0
  PropAnglerType 1
  PropAnglerSpeed 0.10
  PropAnglerMinParam 1666.665
  PropAnglerMaxParam 3000.0
  PropAnglerAfterburnerParam 3010.0
  PropPhiMin 15.0                          // 21.5
  PropPhiMax 45.0                          // 51.5
  PropAoA0 11.0
  Voptimal 320.0
  cCompressor 0  
  CompressorType 1
  CompressorSteps 1
  CompressorPAt0 0.40
  CompressorRPMCurvature 5.0
  CompressorPMax 1.79
  CompressorAltitude0 3292.0
  CompressorMultiplier0 1.0
  CompressorBaseMultiplier0 1.022586207  
  CompressorRPMP0 2000.0
  CompressorRPMPMax 3010.0
  CompressorMaxATARPM 1.56677
  CompressorSpeedManifold 0.8
  CompressorRPM0 400
  CompressorATA0 0.55
  CompressorRPM1 1200
  CompressorATA1 0.70
  CompressorRPM2 2000
  CompressorATA2 1.00
  CompressorRPM3 2280
  CompressorATA3 1.07
  CompressorRPM4 2600
  CompressorATA4 1.28
  CompressorRPM5 3000
  CompressorATA5 1.56677
  DisP0x 3000
  DisP0y 0
  DisP1x 0
  DisP1y 50
  TESPEED 0.01
  TWATERMAXRPM 85
  TOILINMAXRPM 60
  TOILOUTMAXRPM 80
  MAXRPMTIME 400
  MINRPMTIME 999
  TWATERMAX 125
  TWATERMIN 60
  TOILMAX 100
  TOILMIN 40

http://www.wwiiaircraftperformance.o...A-Addendum.pdf
http://www.wwiiaircraftperformance.o...-19-1325-A.pdf
http://www.wwiiaircraftperformance.o...-19-1385-A.pdf