Analysis methods for novel cargo aircraft concepts:
Gespeichert in:
| 1. Verfasser: | |
|---|---|
| Format: | Buch |
| Sprache: | English |
| Veröffentlicht: |
München
Verl. Dr. Hut
2002
|
| Ausgabe: | 1. Aufl. |
| Schriftenreihe: | Luftfahrt
|
| Schlagworte: | |
| Online-Zugang: | Inhaltsverzeichnis |
| Beschreibung: | Zugl.: München, Techn. Univ., Diss., 2002 |
| Beschreibung: | VI, 142 S. Ill., graph. Darst. : 21 cm |
| ISBN: | 3934767516 |
Internformat
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| 245 | 1 | 0 | |a Analysis methods for novel cargo aircraft concepts |c Shengjing Tang |
| 250 | |a 1. Aufl. | ||
| 264 | 1 | |a München |b Verl. Dr. Hut |c 2002 | |
| 300 | |a VI, 142 S. |b Ill., graph. Darst. : 21 cm | ||
| 336 | |b txt |2 rdacontent | ||
| 337 | |b n |2 rdamedia | ||
| 338 | |b nc |2 rdacarrier | ||
| 490 | 0 | |a Luftfahrt | |
| 500 | |a Zugl.: München, Techn. Univ., Diss., 2002 | ||
| 650 | 4 | |a Aeronautics, Commercial |x Freight | |
| 650 | 4 | |a Airplanes |x Design and construction | |
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Datensatz im Suchindex
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| adam_text |
CONTENTS
ABSTRACT
.
V
1
INTRODUCTION
.
1
1.1
DEMAND
FOR
FREIGHTERS
.
1
1.2
A
NEW
AIR
CARGO
SYSTEM
CONCEPT
.
3
1.3
NEW
FREIGHTER
CONCEPTS
.
4
2
OBJECTIVES
.
8
2.1
OUTLINES
.
8
2.2
MODEL
CONSTRUCTION
OF
THE
REFERENCE
CONFIGURATION
.
9
2.3
ESTIMATION
OF
AERODYNAMIC
DATA
DUE
TO
GEOMETRY
.
10
2.4 DYNAMIC
STABILITY
ANALYSIS
.
10
3
REFERENCE
MODEL
AND
COMPUTER
AIDED
GEOMETRY
DESIGN
.
12
3.1
ECOLIFTER
REFERENCE
MODEL
.
12
3.1.1
BRIEF
DESCRIPTION
.
12
3.1.2
THREE
VIEW
SKETCH
AND
TECHNICAL
DATA
.
12
3.2
COMPUTER
AIDED
GEOMETRY
DESIGN
OF
ECOLIFTER
.
13
3.2.1
BASIC
GEOMETRY
CONSTRUCTION
.
13
3.2.2
GEOMETRIC
DESIGN
OF
BASIC
COMPONENTS
.
14
3.2.3
RESULTS
OF
GEOMETRY
VISUALIZATION
.
16
3.3
SUMMARY
.
17
4
ESTIMATION
OF
AERODYNAMIC
DATA
FOR
ECOLIFTER
.
18
4.1
BRIEF
INTRODUCTION
TO
STANDARD
ATMOSPHERE
.
18
4.2 FLIGHT
CONDITIONS
.
19
4.2.1
IN
CRUISE
CONDITION
.
19
4.2.2
IN
APPROACH
CONDITION
.
19
4.3
BRIEF
INTRODUCTION
TO
ESTIMATION
METHOD
.
20
4.3.1
DRAG
COEFFICIENT
C
D
.
20
4.3.2
LIFT
COEFFICIENT
C
L
.
20
4.3.3
PITCHING
MOMENT
COEFFICIENT
C
M
.
21
4.3.4
STABILITY
AND
CONTROL
DERIVATIVES
.
22
4.4
ESTIMATION
RESULTS
OF
AERODYNAMIC
COEFFICIENTS
AND
DERIVATIVES
.
22
4.4.1
DRAG
POLAR
AND
LIFT
TO
DRAG
RATIO
IN
CLEAN
CONFIGURATION
.
22
4.4.2
AIRPLANE
LIFT
COEFFICIENT
C
L
.
24
4.4.3
AIRPLANE
PITCHING
MOMENT
COEFFICIENT
CM
.
25
4.4.4
AERODYNAMIC
COEFFICIENTS,
STABILITY
AND CONTROL
DERIVATIVES
.
26
4.5
SUMMARY
.
30
5
WEIGHT
BREAK
DOWN
AND
MASS
DISTRIBUTION
.
31
5.1
PAY
LOAD
DECOMPOSITION
.
31
5.2
PROPULSION
ESTIMATION
.
32
5.2.1
THRUST-TO-WEIGHT
RATIO
.
32
5.2.2
TAKE-OFF
THRUST
.
32
5.2.3
SELECTION
OF
ENGINE
TYPE
.
33
5.3
OWE
COMPONENTS
BREAK
DOWN
.
33
5.3.1
AIRPLANE
STRUCTURE
.
33
5.3.2
AIRPLANE
EQUIPMENT
.
36
5.3.3
OPERATIONAL
ITEMS
.
37
5.3.4
RESULTS
OF
THE
OWE
COMPONENTS
BREAK
DOWN
.
37
5.4
CENTRE
OF
GRAVITY
.
38
5.4.1
ESTIMATION
OF
CENTRE
OF
GRAVITY
.
38
5.4.2
ESTIMATION
RESULTS
OF
CG
AND
MTOW
.
45
5.4.3
VARIATION
OF
CG
WITH
TYPICAL
WEIGHTS
.
48
5.5
ESTIMATION
OF
MOMENTS
AND
PRODUCTS
OF
INERTIA
.
48
5.5.1
BASIC
FORMULAE
OF
MOMENTS
AND
PRODUCTS
OF
INERTIA
.
49
5.5.2
INERTIA
OF
MAIN
COMPONENTS
ABOUT
THEIR
OWN
CENTRE
OF
GRAVITY
.
50
5.5.3
RESULTS
OF
MOMENTS
AND
PRODUCTS
OF
INERTIA
.
53
5.6
SUMMARY
.
53
6
DYNAMIC
STABILITY
ANALYSIS
ON
ECOLIFTER
.
54
6.1
CHARACTERISTIC
EQUATIONS
OF
ECOLIFTER
.
54
6.1.1
CHARACTERISTIC
EQUATIONS
.
54
6.1.2
ROOTS
OF
CHARACTERISTIC
EQUATIONS
.
56
6.2
VALIDATION
OF
STABILITY
PROGRAM
.
57
6.2.1
COMPARISON
OF
THE
RESULTS
OF
LONGITUDINAL
MOTION
.
57
6.2.2
RESULTS
OF
LATERAL-DIRECTIONAL
MOTION
.
58
6.2.3
CONCLUSION
.
58
6.3
DYNAMIC
STABILITY
OF
ECOLIFTER
.
59
6.3.1
DYNAMIC
STABILITY
OF
ECOLIFTER
IN
CRUISE
CONDITION
.
59
6.3.2
AIRPLANE
SYSTEM
RESPONSE
TO
THE
UNIT
STEP
OF
CONTROL
DEFLECTION
.
62
6.3.3
DYNAMIC
STABILITY
OF
ECOLIFTER
IN
APPROACH
CONDITION
.
65
6.4
SUMMARY
.
68
7
SENSITIVITY
ANALYSES
OF
DYNAMIC
STABILITY
AND
CONFIGURATION
CHANGES
.
69
7.1
VARIATION
OF
DYNAMIC
STABILITY
WITH
FLIGHT
ALTITUDES
.
69
7.1.1
VARIATIONS
OF
ATMOSPHERIC
PARAMETERS
WITH
DIFFERENT
ALTITUDES
.
69
7.1.2
EFFECTS
OF
FLIGHT
ALTITUDES
ON
THE
ROOT
LOCUS
.
70
7.1.3
EFFECTS
OF
FLIGHT
ALTITUDES
ON
DAMPING
AND
FREQUENCIES
.
72
7.2
VARIATION
OF
DYNAMIC
STABILITY
WITH
CANARD
PARAMETERS
.
74
7.2.1
EFFECTS
OF
CANARD
AERODYNAMIC
CENTRE
POSITION
ON
DYNAMIC
STABILITY
.
74
7.2.2
EFFECTS
OF
CANARD
AREA
ON
DYNAMIC
STABILITY
.
76
7.3
VARIATION
OF
DYNAMIC
STABILITY
WITH
HORIZONTAL
TAIL
PARAMETERS
.
78
7.3.1
EFFECTS
OF
HORIZONTAL
TAIL
AERODYNAMIC
CENTRE
VARIATION
ON
DYNAMIC
STABILITY.
78
7.3.2
EFFECTS
OF
HORIZONTAL
TAIL
AREA
ON
DYNAMIC
STABILITY
.
81
7.4
VARIATION
OF
DYNAMIC
STABILITY
WITH
WING
AREA
.
83
7.4.1
VARIATIONS
OF
WING
AREA
.
83
7.4.2
EFFECTS
OF
WING
AREA
ON
LONGITUDINAL
MOTION
.
83
7.4.3
EFFECTS
OF
WING
AREA
ON
LATERAL-DIRECTIONAL
MOTION
.
84
7.5
VARIATION
OF
DYNAMIC
STABILITY
WITH
CENTRE
OF
GRAVITY
.
85
7.5.1
VARIATIONS
OF
AIRPLANE
CENTRE
OF
GRAVITY
.
85
7.5.2 EFFECTS
OF
CENTRE
OF
GRAVITY
ON
LONGITUDINAL
MOTION
.
87
7.5.3
EFFECTS
OF
CENTRE
OF
GRAVITY
ON
LATERAL-DIRECTIONAL
MOTION
.
89
7.6
VARIATION
OF
DYNAMIC
STABILITY
WITH
ENGINE
POSITION
.
89
7.6.1
CASE
1
OF
ENGINE
POSITION
.
89
7.6.2
CASE
2
OF
ENGINE
POSITION
.
90
7.6.3
CASE
3
OF
ENGINE
POSITION
.
92
7.7
SUMMARY
.
93
8
EFFECTS
OF
UPWASH
AND
DOWNWASH
ON
AERODYNAMIC
DATA
.
94
8.1
VARIATIONS
OF
UPWASH
AND
DOWNWASH
GRADIENT
.
94
DE
8.1.1
VARIATION
OF
UPWASH
GRADIENT
-
-
.
94
DA
-
II
-
8.1.2
VARIATION
OF
DOWNWASH
GRADIENT
-
.
95
DA
8.2
EFFECT
OF
CANARD
ON
AIRPLANE
LIFT
COEFFICIENT
.
96
8.2.1
LIFT
CURVE
SLOPE
OF
CANARD
VERSUS
MACH
NUMBER
.
96
8.2.2
EFFECT
OF
CANARD
ON
AIRPLANE
LIFT
CURVE
SLOPE
.
96
8.2.3
EFFECT
OF
CANARD
ON
AIRPLANE
ZERO-ANGLE-OF-ATTACK
LIFT
COEFFICIENT
.
97
8.2.4
CANARD
LIFT
COEFFICIENT
VERSUS
A
AND
I
C
.
98
8.3
EFFECT
OF
CANARD
ON
PITCHING
MOMENT
COEFFICIENT
.
99
8.3.1
EFFECT
OF
CANARD
ON
AIRPLANE
ZERO-LIFT
PITCHING
MOMENT
COEFFICIENT
.
99
8.3.2
EFFECT
OF
CANARD
ON
PITCHING
MOMENT
VARIATION
WITH
LIFT
COEFFICIENT
.
99
8.4
EFFECT
OF
CANARD
ON
STABILITY
DERIVATIVES
.
100
8.4.1
EFFECT
OF
CANARD
ON
LIFT-DUE-TO-PITCH-RATE
DERIVATIVE
.
100
8.4.2
EFFECT
OF
CANARD
ON
PITCHING-MOMENT-DUE-TO-PITCH-RATE
DERIVATIVE
.
101
8.4.3
EFFECT
OF
CANARD
ON
PITCHING
MOMENT
DUE
TO
A
.
102
8.5
EFFECT
OF
CANARD
ON
CONTROL
DERIVATIVES
.
102
8.6
SUMMARY
.
103
9
DISCUSSION
OF
RESULTS
.
104
9.1
MODELLING
.
104
9.2
ESTIMATION
OF
AERODYNAMICS
OF
ECOLIFTER
.
105
9.3
DYNAMIC
STABILITY
ANALYSIS
ON
ECOLIFTER
.
107
9.4
SENSITIVITY
ANALYSES
ON
DYNAMIC
STABILITY
OF
ECOLIFTER
.
109
9.5
INTEGRATED
RESEARCH
IN
CONCEPTUAL
DESIGN
.
114
9.5.1
PARAMETER
VARIATION
IN
INTEGRATED
CONCEPTUAL
DESIGN
.
115
9.5.2
EXAMPLE
FOR
A
DYNAMIC
STABILITY
IMPROVEMENT
.
116
9.6
SUMMARY
.
117
10
SUMMARY
AND
CONCLUSIONS
.
119
11
REFERENCES
.
122
APPENDIX
1:
SYMBOLS,
NOTATION
AND
ABBREVIATIONS
.
129
APPENDIX
2:
THREE
VIEW
SKETCH
AND
TECHNICAL
DATA
OF
ECOLIFTER
.
139
APPENDIX
3:
LINEARIZED
SMALL
PERTURBATION
EQUATIONS
OF
MOTION
.
142
-
III
- |
| any_adam_object | 1 |
| author | Tang, Shengjing |
| author_facet | Tang, Shengjing |
| author_role | aut |
| author_sort | Tang, Shengjing |
| author_variant | s t st |
| building | Verbundindex |
| bvnumber | BV014201326 |
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| callnumber-label | TL671 |
| callnumber-raw | TL671.2 |
| callnumber-search | TL671.2 |
| callnumber-sort | TL 3671.2 |
| callnumber-subject | TL - Motor Vehicles and Aeronautics |
| classification_tum | VER 570d VER 600d |
| ctrlnum | (OCoLC)52995177 (DE-599)BVBBV014201326 |
| discipline | Verkehrstechnik |
| edition | 1. Aufl. |
| format | Book |
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| genre_facet | Hochschulschrift |
| id | DE-604.BV014201326 |
| illustrated | Illustrated |
| indexdate | 2024-08-24T00:33:27Z |
| institution | BVB |
| isbn | 3934767516 |
| language | English |
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| physical | VI, 142 S. Ill., graph. Darst. : 21 cm |
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| publisher | Verl. Dr. Hut |
| record_format | marc |
| series2 | Luftfahrt |
| spelling | Tang, Shengjing Verfasser aut Analysis methods for novel cargo aircraft concepts Shengjing Tang 1. Aufl. München Verl. Dr. Hut 2002 VI, 142 S. Ill., graph. Darst. : 21 cm txt rdacontent n rdamedia nc rdacarrier Luftfahrt Zugl.: München, Techn. Univ., Diss., 2002 Aeronautics, Commercial Freight Airplanes Design and construction Räumliche Anordnung (DE-588)4344368-0 gnd rswk-swf Frachtflugzeug (DE-588)4456889-7 gnd rswk-swf Systementwurf (DE-588)4261480-6 gnd rswk-swf (DE-588)4113937-9 Hochschulschrift gnd-content Frachtflugzeug (DE-588)4456889-7 s Systementwurf (DE-588)4261480-6 s Räumliche Anordnung (DE-588)4344368-0 s DE-604 DNB Datenaustausch application/pdf http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=009735527&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA Inhaltsverzeichnis |
| spellingShingle | Tang, Shengjing Analysis methods for novel cargo aircraft concepts Aeronautics, Commercial Freight Airplanes Design and construction Räumliche Anordnung (DE-588)4344368-0 gnd Frachtflugzeug (DE-588)4456889-7 gnd Systementwurf (DE-588)4261480-6 gnd |
| subject_GND | (DE-588)4344368-0 (DE-588)4456889-7 (DE-588)4261480-6 (DE-588)4113937-9 |
| title | Analysis methods for novel cargo aircraft concepts |
| title_auth | Analysis methods for novel cargo aircraft concepts |
| title_exact_search | Analysis methods for novel cargo aircraft concepts |
| title_full | Analysis methods for novel cargo aircraft concepts Shengjing Tang |
| title_fullStr | Analysis methods for novel cargo aircraft concepts Shengjing Tang |
| title_full_unstemmed | Analysis methods for novel cargo aircraft concepts Shengjing Tang |
| title_short | Analysis methods for novel cargo aircraft concepts |
| title_sort | analysis methods for novel cargo aircraft concepts |
| topic | Aeronautics, Commercial Freight Airplanes Design and construction Räumliche Anordnung (DE-588)4344368-0 gnd Frachtflugzeug (DE-588)4456889-7 gnd Systementwurf (DE-588)4261480-6 gnd |
| topic_facet | Aeronautics, Commercial Freight Airplanes Design and construction Räumliche Anordnung Frachtflugzeug Systementwurf Hochschulschrift |
| url | http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=009735527&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA |
| work_keys_str_mv | AT tangshengjing analysismethodsfornovelcargoaircraftconcepts |