Cessna 525 Citation Jet

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Advanced Aircraft Analysis

Cessna 525 Citation Jet

Chapter 1: Flight condition

1.1 Flight condition

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1.2 Atmosphere

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Chapter 2: Geometry

2.1 Wing

2.1.1 Straight Tapered

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2.1.2 Cranked wing

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2.1.3 Aileron

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2.2 Horiontal !ale

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2." #ertical !ail2.3.1 Straight Tapered

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2.3.2 Rudder

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2.$ F%selage

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2.5 &anding Gear

Chapter " : Weight

".1 Weight siing

3.1.1 Mission Profile

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3.1.2 Take-off Weight

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3.1.3 Regression

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3.1. Sensiti!it"

3.2 Class ' Weight

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3.3 Class '' Weight

".".1 (tr%ct%re

3.3.1.1 Wing

3.3.1.2 #erti$al Tail

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3.3.1.3 %anding &ear

3.3.1.3.1 'ose &ear

3.3.1.3.2 Main &ear

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3.3.1.3.3 Total &ear

3.3.1. (ori)ontal Tale

3.3.1.* +uselage

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3.3.1., 'a$elle

3.3.1. Total stru$ture

".".2 )o*erplant

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3.3.2.1 ngine

3.3.2.2 +uel s"ste/

3.3.2.3 Air indu$tion

3.3.2. Propulsion s"ste/

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3.3.2. Total Powerplant

"."." !otal Weight

".$ Center of Gravity

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Chapter $ : Aerodynamics$.1 &ift.1.1 Wing

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.1.2 (ori)ontal Tale

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.1.3 #erti$al Tale

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.1..1 +lap si)ing

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.1..2 +lap lift

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.1.* Airplane %ift

.1.*.1 Tri//ed %ift

.1.*.2 0ntri//ed %ift

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$.2 +rag

.2.1 Class drag.2.1.1 Take-off &ear down

.2.1.2 Take-off &ear up

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.2.1.3 %anding &ear up

.2.1. %anding &ear down

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.2.1.* Clean

.2.1., ne ngine noperati!e

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.2.1. Current +light Condition

.2.1.4 All polars

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$.2.2 Class '' +rag.2.2.1 Tri//ed plot

.2.2.1.1 5rag polars for $onstant Ma$h nu/6er

.2.2.1.2 CD - M $ur!es for $onstant lift $oeffi$ient

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.2.2.1.3 5rag polars 6uilt up of different drag $o/ponents

.2.2.1. CD- $ur!es

.2.2.2 0ntri//ed plot

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.2.2.2.1 5rag polars for $onstant Ma$h nu/6er

.2.2.2.2 CD - M $ur!es for $onstant lift $oeffi$ient

.2.2.2.3 5rag polars 6uilt up of different drag $o/ponents

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$." ,oment.3.1 Wing

.3.2 (ori)ontal Tail

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.3.3 #erti$al Tail

.3. Airplane

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$.$ Aerodynamic Center

$.5 Gro%nd -ffects

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$. +ynamic )ress%re /atio

Chapter 5: )erformance

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5.1 )erformance (iing

5.2 )erformance Analysis

*.2.1 Thrust-Speed Perfor/an$e Cur!e

*.2.2 Clim0

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5.2." +ive +escent

*.2. &lide

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Chapter : )rop%lsion

.1 'nlet area siing

Chapter : (ta0ility and Control

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.1 +erivatives.1.1 %ongitudinal sta6ilit" deri!ati!es

.1.1.1 Stead" state $oeffi$ients

.1.1.2 Speed 5eri!ati!es

.1.1.3 Angle-of-Atta$k 5eri!ati!es

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.1.1. Rate of Angle-of-Atta$k 5eri!ati!es

.1.1. Pit$h Rate 5eri!ati!es

.1.1. Pit$h Rate 5eri!ati!es

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.1.2 %ateral-5ire$tional Sta6ilit" 5eri!ati!es

.1.2.1 Sideslip

.1.2.2 Sideslip Rate

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.1.2.3 Roll Rate

.1.2. 7aw Rate

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.1." &ongit%dinal Control

.1.3.1 Sta6ili)er

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.1.3.2 le!ator

%ift due to ele!ator defle$tion

Mo/ent due to ele!ator defle$tion

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.1.3.3 le!ator Ta6

.1.$ &ateral3+irectional Control +erivatives.1.$.1 Aileron /elated +erivatives

Rolling-/o/ent $oeffi$ient-due-to-aileron deri!ati!e.

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7awing-/o/ent $oeffi$ient-due-to-aileron deri!ati!e.

.1.$.2Aileron !a0 /elated +erivatives

.1.$." /%dder !a0 /elated +erivatives

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.2 Analysis.2.1 Clas '' !rim analysis.2.1.1 !rim diagram

.2.1.2 &ongit%dinal trim

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.2.1." &ateral +irectional trim

.2.2 !rim lift coefficients

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Chapter 4: +ynamics

4.1 ode method

Chapter 6: &oads6.1 #3n +iagram