12/24/2014 F­15 Aerodynamic data from (AFIT/GAE/ENY/90D­16); CG 25.65%

http://localhost:57242/Plots.aspx 1/21

F­15 Aerodynamic data from (AFIT/GAE/ENY/90D­16); CG25.65%

LIFT

12/24/2014 F­15 Aerodynamic data from (AFIT/GAE/ENY/90D­16); CG 25.65%

http://localhost:57242/Plots.aspx 2/21

12/24/2014 F­15 Aerodynamic data from (AFIT/GAE/ENY/90D­16); CG 25.65%

http://localhost:57242/Plots.aspx 3/21

DRAG

12/24/2014 F­15 Aerodynamic data from (AFIT/GAE/ENY/90D­16); CG 25.65%

http://localhost:57242/Plots.aspx 4/21

12/24/2014 F­15 Aerodynamic data from (AFIT/GAE/ENY/90D­16); CG 25.65%

http://localhost:57242/Plots.aspx 5/21

SIDE

12/24/2014 F­15 Aerodynamic data from (AFIT/GAE/ENY/90D­16); CG 25.65%

http://localhost:57242/Plots.aspx 6/21

12/24/2014 F­15 Aerodynamic data from (AFIT/GAE/ENY/90D­16); CG 25.65%

http://localhost:57242/Plots.aspx 7/21

12/24/2014 F­15 Aerodynamic data from (AFIT/GAE/ENY/90D­16); CG 25.65%

http://localhost:57242/Plots.aspx 8/21

12/24/2014 F­15 Aerodynamic data from (AFIT/GAE/ENY/90D­16); CG 25.65%

http://localhost:57242/Plots.aspx 9/21

12/24/2014 F­15 Aerodynamic data from (AFIT/GAE/ENY/90D­16); CG 25.65%

http://localhost:57242/Plots.aspx 10/21

ROLL

12/24/2014 F­15 Aerodynamic data from (AFIT/GAE/ENY/90D­16); CG 25.65%

http://localhost:57242/Plots.aspx 11/21

12/24/2014 F­15 Aerodynamic data from (AFIT/GAE/ENY/90D­16); CG 25.65%

http://localhost:57242/Plots.aspx 12/21

PITCH

12/24/2014 F­15 Aerodynamic data from (AFIT/GAE/ENY/90D­16); CG 25.65%

http://localhost:57242/Plots.aspx 13/21

12/24/2014 F­15 Aerodynamic data from (AFIT/GAE/ENY/90D­16); CG 25.65%

http://localhost:57242/Plots.aspx 14/21

YAW

12/24/2014 F­15 Aerodynamic data from (AFIT/GAE/ENY/90D­16); CG 25.65%

http://localhost:57242/Plots.aspx 15/21

12/24/2014 F­15 Aerodynamic data from (AFIT/GAE/ENY/90D­16); CG 25.65%

http://localhost:57242/Plots.aspx 16/21

12/24/2014 F­15 Aerodynamic data from (AFIT/GAE/ENY/90D­16); CG 25.65%

http://localhost:57242/Plots.aspx 17/21

12/24/2014 F­15 Aerodynamic data from (AFIT/GAE/ENY/90D­16); CG 25.65%

http://localhost:57242/Plots.aspx 18/21

12/24/2014 F­15 Aerodynamic data from (AFIT/GAE/ENY/90D­16); CG 25.65%

http://localhost:57242/Plots.aspx 19/21

Lift Coefficient BuildupLIFT=CFZB+ClUC*gear/gear­pos­norm+ClDFM+DClRamp*propulsion/inlet/ramp1­position­norm *ClMach

Drag Coefficient BuildupDRAG=CFXB+CdUC*gear/gear­pos­norm+CdDBRK*fcs/speedbrake­pos­norm+CdDFM+CdTNK*fcs/external­tanks­fitted+DCdRamp*propulsion/inlet/ramp1­position­norm *CdMach

Side Coefficient BuildupSIDE=CFYB+CYDAD*DDA+CYDRD*DRUDD*DRFLX5*EPA43+CYDTD*DTFLX5*0.3*DTALD+CYRB+CFYP*PB+CFYR*RB *CyMach

Roll Coefficient BuildupROLL=CML1+CMLDAD*DDA+CMLDRD*DRUDD*DRFLX1*EPA43+CMLDTD*DTFLX1*0.3*DTALD+CMLP*PB+CMLR*RB+CMLDCLB*BETA*metrics/two­place­canopy *CLMach + (DLNB*BETA)

Pitch Coefficient BuildupPITCH=CMM1+CMMQ*QB+DCMAIM*fcs/aim­fitted+CMUC*gear/gear­pos­norm+CMDFM+DCMRamp*propulsion/inlet/ramp1­position­norm *CMMach

Yaw Coefficient BuildupYAW=CMN1+CMNDAD*DDA+CMNDRDr*DRUDD*DRFLX3*EPA43+CMNDTD*DTFLX3*0.3*DTALD+CMNP*PB+CMNR*RB+CMNRB *CNMach +(DCNB*BETA)

References1. Richard Harrison, rjh@zaretto.com: F­15 Aerodynamic data from (AFIT/GAE/ENY/90D­16); CG 25.65%, ZDAT/AED/2014/12­2, December,

2014: http://www.zaretto.com/sites/zaretto.com/files/F­15­data/rjh­zaretto­f­15­aerodynamic­data.pdf(http://www.zaretto.com/sites/zaretto.com/files/F­15­data/rjh­zaretto­f­15­aerodynamic­data.pdf)

2. Robert J. McDonnell, B.S., Captain, USAF: INVESTIGATION OF THE HIGH ANGLE OF ATTACK DYNAMICS OF THE F­15B USINGBIFURCATION ANALYSIS, AFIT/GAE/ENY/90D­16, December 1990: http://www.zaretto.com/sites/zaretto.com/files/F­15­data/ADA230462.pdf(http://www.zaretto.com/sites/zaretto.com/files/F­15­data/ADA230462.pdf)

3. Richard L. Bennet, Major, USAF: ANALYSIS OF THE EFFECTS OF REMOVING NOSE BALLAST FROM THE F­15 EAGLE, AFIT/GA/ENY/91D­1, December 1991: http://www.zaretto.com/sites/zaretto.com/files/F­15­data/ADA244044.pdf (http://www.zaretto.com/sites/zaretto.com/files/F­15­data/ADA244044.pdf)

4. DR. J. R. LUMMUS, G. T. JOYCE, O C. D. O MALLEY: ANALYSIS OF WIND TUNNEL TEST RESULTS FOR A 9.39­PER CENT SCALE MODELOF A VSTOL FIGHTER/ATTACK AIRCRAFT : VOLUME I ­ STUDY OVERVIEW, NASA CR­152391­VOL­1 Figure 3­2 p54, October 1980:http://www.zaretto.com/sites/zaretto.com/files/F­15­data/19810014497.pdf (http://www.zaretto.com/sites/zaretto.com/files/F­15­

12/24/2014 F­15 Aerodynamic data from (AFIT/GAE/ENY/90D­16); CG 25.65%

http://localhost:57242/Plots.aspx 20/21

data/19810014497.pdf)5. Frank W. Burcham, Jr., Trindel A. Maine, C. Gordon Fullerton, and Lannie Dean Webb: Development and Flight Evaluation of an Emergency

Digital Flight Control System Using Only Engine Thrust on an F­15 Airplane, NASA TP­3627, September 1996:http://www.zaretto.com/sites/zaretto.com/files/F­15­data/88414main_H­2048.pdf (http://www.zaretto.com/sites/zaretto.com/files/F­15­data/88414main_H­2048.pdf)

Mass and balanceElement X Y Z Unit

Aerodynamic Reference Point (CoP) 457.07 0.00 0.00 IN

Aircraft CG 408.00 0.00 0.00 IN

Ground ReactionsElement X Y Z Unit

NOSE_LG 197.00 0.00 ­77.65 IN

LEFT_MLG 451.00 ­98.00 ­84.34 IN

RIGHT_MLG 451.00 98.00 ­84.34 IN

LEFT_WING_TIP 472.00 ­256.80 13.00 IN

RIGHT_WING_TIP 472.00 256.80 13.00 IN

CANOPY 214.00 0.00 10.00 IN

RADOME_FRONT 20.00 0.00 ­18.00 IN

LEFT_VERTICAL_TAIL 744.00 ­98.00 60.00 IN

RIGHT_VERTICAL_TAIL 744.00 98.00 60.00 IN

REAR_BODY_LEFT 669.00 ­58.00 ­12.00 IN

REAR_BODY_RIGHT 669.00 58.00 ­12.00 IN

NOSE_CONE 0.00 0.00 ­15.00 IN

PropulsionElement X Y Z Unit Feed

F100­PW­229

682.00 ­12.00 0.00 IN External Tank [0],Tank 1 [1],Left Wing Tank [2],Left Engine Feed [4],Left External Wing Tank [6],LeftFeed line [8]

F100­PW­229

682.00 12.00 0.00 IN External Tank [0],Tank 1 [1],Right Wing Tank [3],Right Engine Feed [5],Right External Wing Tank[7],Right Feed line [9]

TanksElement X Y Z Unit Capacity Id Priority

External Tank 450.00 0.00 ­7.83 IN 3950 LBS 0 1

Tank 1 422.00 0.00 ­5.77 IN 3300 LBS 1 2

Left Wing Tank 450.00 0.00 ­7.83 IN 2750 LBS 2 3

12/24/2014 F­15 Aerodynamic data from (AFIT/GAE/ENY/90D­16); CG 25.65%

http://localhost:57242/Plots.aspx 21/21

Right Wing Tank 450.00 0.00 ­7.83 IN 2750 LBS 3 3

Left Engine Feed 430.00 0.00 ­7.83 IN 1200 LBS 4 4

Right Engine Feed 430.00 0.00 ­7.83 IN 1500 LBS 5 4

Left External Wing Tank 450.00 0.00 ­7.83 IN 3950 LBS 6 5

Right External Wing Tank 450.00 0.00 ­7.83 IN 3950 LBS 7 5

Left Feed line 454.00 ­38.00 ­47.00 IN 10 LBS 8 6

Right Feed line 454.00 38.00 ­47.00 IN 10 LBS 9 6