Root Tip
------------ -----------
Fokker 100 Fokker 12.3% Fokker 9.6%
Fokker 50 NACA 64-421 NACA 64-415
Fokker 60 NACA 64-421 NACA 64-415
Fokker 70 Fokker 12.3% Fokker 9.6%
-------------------------------------------------------------------------------
http://rahauav.com/Library/Aerodynamic/Aerodynamic_design_of_transport_aircraft_www.rahaUAV.com.pdf
Aerodynamic Design of Transport Aircraft
Figure 27.14 Tail-Off lift curves for the Fokker 100
(Source: Fokker Rep. A-166 and A-173
alpha flaps (deg)
(deg) 0 20 42
0.0 0.22 0.84 1.27
10.0 1.11 1.70 2.17
12.0 1.27 1.83 2.31
14.0 1.40 1.72 1.90
16.0 1.34 0.71 0.00
Figure 27.23 Drag due to flap deflection at three angles of attack, Fokker 100
(Source: Fokker Rep. A-166 and A-173)
alpha flaps (deg)
(deg) 0 20 42
-4.0 0.0000 0.0047 0.0156
0.0 0.0000 0.0070 0.0200
2.0 0.0001 0.0077 0.0225
4.0 0.0005 0.0089 0.0257
6.0 0.0008 0.0129 0.0276
8.0 0.0025 0.0156 0.0313
Figure 33.9 Comparison of aileron effectiveness from wind tunnel and
flight tests - Fokker F-28 Mk 1000
(Source: Fokker report V-28-75)
Clda flaps (deg)
Mach 10 20
0.60 -0.022 -0.043
0.65 -0.022 -0.037
0.70 -0.023 -0.027
0.75 -0.019 -0.027
0.80 -0.015 -0.026
-------------------------------------------------------------------------------
Advanced Topics in Aerodynamics, Aerodynamic Database (AD)
http://aerodyn.org/HighLift/tables.html
---
CLmax 3.45 (in ground effect)
-------------------------------------------------------------------------------
Butterworth-Heinemann - Civil Jet Aircraft Design
http://booksite.elsevier.com/9780340741528/appendices/data-a/default.htm
http://booksite.elsevier.com/9780340741528/appendices/data-a/table-8/table.htm
---
CLmax (t/o) 2.17 (Df = 15 degrees)
CLmax (l/d@MLM) 2.59 (Df = 42 degrees)
-------------------------------------------------------------------------------
Lissys - Piano-X output:
http://www.lissys.demon.co.uk/f7tx2.html
(Note: Simulated Fokker 70 data)
---
CLmax (t/o) 1.91 (Df = 0 degrees)
L/D (2nd sgement) 12.54 (incl. windmill. & asymm).
CLmax (l/d) 2.43 (Df = 42 degrees)
L/D (approach) 4.91 (gear down)
AERODYNAMIC DRAG REPORT (Altitude: 0ft)
-------------------------------------------------------
MACH CD0 CDi CDmach CDtrim CDtotal| CL | SFC
----- ------- ------- ------- ------- -------|-----|------
0.212 0.02035 0.05398 0.00190 -.00011 0.07613|1.099|0.7209
0.230 0.02013 0.04096 0.00000 0.00013 0.06122|0.957|0.7520
0.272 0.01957 0.01975 0.00000 0.00042 0.03975|0.665|0.8105
0.302 0.01925 0.01296 0.00000 0.00047 0.03268|0.539|0.8341
0.378 0.01857 0.00531 0.00000 0.00045 0.02432|0.345|0.8575
0.454 0.01801 0.00256 0.00000 0.00039 0.02096|0.239|0.8627
0.600 0.01712 0.00083 0.00000 0.00030 0.01826|0.137|0.8574
0.800 0.01614 0.00027 0.00373 0.00023 0.02036|0.077|0.8552
0.840 0.01596 0.00022 0.01067 0.00022 0.02707|0.070|0.8909
0.860 0.01587 0.00020 0.01858 0.00021 0.03487|0.067|0.8985
AERODYNAMIC DRAG REPORT (Altitude: 1000ft)
-------------------------------------------------------
MACH CD0 CDi CDmach CDtrim CDtotal| CL | SFC
----- ------- ------- ------- ------- -------|-----|------
0.653 0.01691 0.00064 0.00026 0.00028 0.01809|0.120|0.8476
0.771 0.01633 0.00033 0.00201 0.00024 0.01891|0.086|0.8524
0.800 0.01620 0.00028 0.00373 0.00023 0.02045|0.080|0.8516
AERODYNAMIC DRAG REPORT (Altitude: 35000ft)
-------------------------------------------------------
MACH CD0 CDi CDmach CDtrim CDtotal| CL | SFC
----- ------- ------- ------- ------- -------|-----|------
0.458 0.02102 0.04432 0.00222 0.00007 0.06763|0.996|0.5924
0.546 0.02034 0.02207 0.00017 0.00040 0.04299|0.703|0.6251
0.603 0.01995 0.01482 0.00036 0.00046 0.03560|0.576|0.6474
0.720 0.01922 0.00867 0.00115 0.00013 0.02917|0.440|0.6908
0.741 0.01910 0.00648 0.00152 0.00046 0.02756|0.381|0.6976
0.768 0.01894 0.00562 0.00251 0.00045 0.02752|0.355|0.7112
0.800 0.01876 0.00478 0.00541 0.00044 0.02939|0.327|0.7392
0.848 0.01855 0.00393 0.01616 0.00042 0.03906|0.296|0.7526
0.860 0.01844 0.00358 0.02737 0.00042 0.04981|0.283|0.7575
-------------------------------------------------------------------------------
Buffet envelope prediction of transport
aircraft during the conceptual design phase
- Predict transonic, shock induced buffet onset
J.N.A. van Eijndhoven BSc
Figure 4.2: Fokker 100 buffet onset flight test
M CL
0.5 1.00
0.55 0.93
0.60 0.88
0.70 0.86
0.75 0.65
0.80 0.52
0.85 0.25
Table 1: dCL for literature and Matrix-V results,
Fokker 100 wing, Λ0.5c at Re ≈ 1.5 · 107
M∞ CLLit [−] CLM atV [−] dCL [−]
0.65 0.86 0.83 0.03
0.68 0.86 0.84 0.02
0.70 0.87 0.85 0.02
0.73 0.72 0.81 -0.09
0.75 0.68 0.71 -0.03
Figure 3.2: Fuselage effect on wing lift distribution
Body Ise Tip
0 0.5 0.75 1.0
CL 0.73 0.7 0.68 0.3
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JSBSim编程实践工程VS2015 (615个子文件)
clean.bat 270B
JSBSimTest.bat 32B
xmlparse.c 185KB
xmltok_impl.c 43KB
xmltok.c 40KB
xmlrole.c 32KB
xmltok_ns.c 3KB
README.flightmodel.c172p 0B
README.c172r 1KB
README.c182 1KB
README.c310 1KB
JSBSim.cpp 11KB
JSBSimTest.cpp 5KB
props.cxx 62KB
strutils.cxx 18KB
sg_path.cxx 16KB
coremag.cxx 13KB
easyxml.cxx 8KB
propertyObject.cxx 2KB
sgstream.cxx 2KB
JSBSimLibTest.exe 1.28MB
prep_plot.vcxproj.filters 3KB
expat.h 39KB
FGLocation.h 30KB
FGInitialCondition.h 29KB
FGPropagate.h 28KB
FGFunction.h 28KB
FGFDMExec.h 27KB
FGPropertyManager.h 26KB
FGStateSpace.h 26KB
FGTrimAnalysis.h 24KB
FGFCS.h 20KB
FGAccelerations.h 19KB
FGQuaternion.h 19KB
FGPiston.h 18KB
FGXMLElement.h 17KB
FGRotor.h 17KB
FGLGear.h 16KB
FGStandardAtmosphere.h 16KB
FGWinds.h 15KB
FGForce.h 14KB
FGMatrix33.h 14KB
FGTank.h 13KB
FGJSBBase.h 13KB
FGTurbine.h 13KB
FGPropeller.h 13KB
FGGasCell.h 13KB
FGAuxiliary.h 13KB
FGMSIS.h 12KB
xmltok.h 11KB
FGAerodynamics.h 11KB
FGAtmosphere.h 11KB
FGTable.h 11KB
FGMassBalance.h 10KB
FGOutput.h 10KB
FGTrim.h 10KB
FGColumnVector3.h 10KB
FGScript.h 9KB
FGGain.h 8KB
FGRocket.h 8KB
FGOutputType.h 8KB
FGPropulsion.h 8KB
FGEngine.h 8KB
FGExternalForce.h 8KB
FGAircraft.h 8KB
FGTurboProp.h 7KB
FGTrimAnalysisControl.h 7KB
nametab.h 7KB
FGBuoyantForces.h 7KB
FGFilter.h 7KB
FGExternalReactions.h 7KB
FGDistributor.h 6KB
FGTransmission.h 6KB
FGSensor.h 6KB
FGSwitch.h 6KB
FGGroundCallback.h 6KB
FGTrimAxis.h 6KB
FGInput.h 6KB
FGActuator.h 6KB
FGFCSChannel.h 5KB
FGInputType.h 5KB
FGRungeKutta.h 5KB
FGGroundReactions.h 5KB
FGPID.h 5KB
FGKinemat.h 5KB
FGOutputFile.h 5KB
FGThruster.h 5KB
FGAccelerometer.h 4KB
string_utilities.h 4KB
FGSurface.h 4KB
FGMagnetometer.h 4KB
FGWaypoint.h 4KB
FGModelFunctions.h 4KB
FGFCSComponent.h 4KB
FGOutputSocket.h 4KB
FGInertial.h 4KB
FGModel.h 4KB
FGSensorOrientation.h 4KB
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资源评论
- zxg_xiaoguang2019-12-28材料不错,可以编译
- SherlockThang2022-01-10还可以吧,还是自己看源码最好,修改CmakeList也不难
- 好好搬砖,快乐生活2024-04-07博主您好! 下载文件不包含JSBSimTest.cpp #内容缺失 #标题与内容不符
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