Flight testing of fixed-wing aircraft:
Gespeichert in:
| 1. Verfasser: | |
|---|---|
| Format: | Buch |
| Sprache: | English |
| Veröffentlicht: |
Reston, VA
American Institute of Aeronautics and Astronautics
2003
|
| Schriftenreihe: | AIAA education series
|
| Schlagworte: | |
| Online-Zugang: | Inhaltsverzeichnis |
| Beschreibung: | Includes bibliographical references and index. |
| Beschreibung: | XVIII, 441 S. Ill., graph. Darst. |
| ISBN: | 1563475642 |
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Datensatz im Suchindex
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| adam_text | FUGHT TESTING OF FIXED-WING AIRCRAFT TU DARMSTADT FB MASCHINENBAU TABLE
OF CONTENTS PREFACE XVII PART 1 PERFORMANCE FLIGHT TESTING CHAPTER 1.
INTRODUCTION 3 1.1 INTRODUCTION TO FLIGHT TESTING 3 1.2 TYPES OF FLIGHT
TESTS 4 1.3 SEQUENCE OF FLIGHT TESTING 4 1.4 PLANNING THE TEST PROGRAM 4
1.5 GOVERNING REQUIREMENTS AND REGULATIONS 6 1.6 THE ATMOSPHERE 9 1.7
AIRCRAFT WEIGHT AND CENTER OF GRAVITY 12 1.8 FLIGHT TESTING TOLERANCES
15 REFERENCES 16 CHAPTER 2. METHODS FOR REDUCING DATA UNCERTAINTY IN
FLIGHT TEST DATA 19 2.1 INTRODUCTION 19 2.2 SOURCES AND MAGNITUDES OF
ERRORS . 19 2.3 AVOIDING OR MINIMIZING ERRORS 22 2.4 ERROR ANALYSIS 25
REFERENCES 28 CHAPTER 3. AIRSPEED SYSTEMS THEORY AND CALIBRATION 29 3.1
INTRODUCTION 29 3.2 FEDERAL AVIATION REGULATION REQUIREMENTS 29 3.3
THEORY OF AIRSPEED SYSTEMS 30 3.4 POSITION ERROR 32 3.5 LAG ERRORS 33
3.6 ALTIMETER POSITION ERROR 33 3.7 IN-FLIGHT CALIBRATION METHODS 34 3.8
TEMPERATURE PROBE CALIBRATION 37 REFERENCES 38 CHAPTER 4. STALL SPEED
MEASUREMENT 39 4.1 INTRODUCTION 39 IX X TABLE OF CONTENTS 4.2 FEDERAL
AVIATION ADMINISTRATION REQUIREMENTS 39 4.3 STALL THEORY 42 4.4 AIRCRAFT
LOADING 47 4.5 SAFETY CONSIDERATIONS 48 4.6 FLIGHT TEST METHOD 48 4.7
DATA REDUCTION METHOD 49 REFERENCES 52 CHAPTER 5. DETERMINATION OF
ENGINE POWER IN FLIGHT S3 5.1 INTRODUCTION 53 5.2 POWER MEASUREMENT OF
AN INTERNAL COMBUSTION ENGINE IN FLIGHT 54 5.3 INSTALLED HORSEPOWER
LOSSES AND HOW THEY AFFECT POWER MEASUREMENT 58 5.4 POWER CORRECTIONS 59
5.5 CRITICAL ALTITUDE DETERMINATION 61 REFERENCES. . * . 62 CHAPTER 6.
PROPELLER THEORY 63 6.1 INTRODUCTION 63 6.2 PROPELLER THEORY 63 6.3
PROPELLER POLAR DIAGRAM 67 6.4 CONSTANT SPEED OR CONTROLLABLE PROPELLERS
67 6.5 ACTIVITY FACTOR 67 6.6 PROPELLER NOISE 68 REFERENCES 68 CHAPTER
7. JET THRUST MEASUREMENT IN FLIGHT 69 7.1 INTRODUCTION 69 7.2 BASIC
THEORY 69 7.3 METHODS OF IN-FLIGHT THRUST MEASUREMENT 72 REFERENCES 74
CHAPTER 8. LEVEL FLIGHT PERFORMANCE THEORY 75 8.1 INTRODUCTION 75 8.2
THRUST REQUIRED 75 8.3 EFFECTS OF VARIABLES ON THRUST REQUIRED 77 8.4
POWER REQUIRED 78 8.5 EFFECTS OF VARIABLES ON THE POWER REQUIRED CURVES
79 8.6 EFFECTS OF HIGH MACH NUMBER 81 8.7 THRUST OR POWER AVAILABLE . .
. . 82 REFERENCES 82 TABLE OF CONTENTS XI CHAPTER 9. LEVEL FLIGHT
PERFORMANCE FLIGHT TEST AND DATA REDUCTION METHODS FOR PROPELLER-DRIVEN
AIRCRAFT 83 9.1 INTRODUCTION 83 9.2 FEDERAL AVIATION ADMINISTRATION
REQUIREMENTS 83 9.3 PIW-VIW METHOD 83 9.4 FLIGHT TEST METHOD 84 9.5
REDUCTION OF OBSERVED DATA 85 9.6 EXPANSION OF OBSERVED DATA 90
REFERENCE 96 CHAPTER 10. LEVEL FLIGHT PERFORMANCE JET AIRCRAFT 97 10.1
INTRODUCTION 97 10.2 THEORY 97 10.3 FLIGHT TEST TECHNIQUES 100 10.4 DATA
REDUCTION 103 REFERENCES 103 CHAPTER 11. RANGE AND ENDURANCE 105 11.1
INTRODUCTION 105 11.2 RANGE*PROPELLER-DRIVEN AIRPLANES 106 11.3
RANGE*JET AIRCRAFT. ILL 11.4 EFFECTS OF WIND ON RANGE 115 11.5
ENDURANCE*PROPELLER-DRIVEN AIRCRAFT 117 11.6 ENDURANCE*JET AIRCRAFT 117
REFERENCES 118 CHAPTER 12. CLIMB PERFORMANCE THEORY 119 12.1
INTRODUCTION 119 12.2 CLIMB THEORY 119 REFERENCES 126 CHAPTER 13. CLIMB
PERFORMANCE METHODS, DATA REDUCTION, AND EXPANSION 127 13.1 INTRODUCTION
127 13.2 FEDERAL AVIATION ADMINISTRATION REGULATIONS 127 13.3 TEST
METHODS 129 13.4 REDUCTION METHODS FOR STEADY CLIMBS 131 13.5 EXPANSION
METHODS 140 REFERENCES 142 CHAPTER 14. ENERGY APPROACH TO PERFORMANCE
FLIGHT TESTING 143 14.1 INTRODUCTION 143 14.2 THEORY 143 14.3
APPLICATION TO CLIMB PERFORMANCE 145 XII TABLE OF CONTENTS 14.4 OTHER
APPLICATIONS OF ENERGY METHODS 147 14.5 LEVEL ACCELERATION FLIGHT TEST
METHOD 149 REFERENCES 151 CHAPTER 15. TURNING PERFORMANCE 153 15.1
INTRODUCTION 153 15.2 FORCES ON AN AIRCRAFT DURING A LEVEL TURN 153 15.3
TURNING PERFORMANCE LIMITATIONS 155 15.4 FLIGHT TEST METHOD 157
REFERENCES 159 CHAPTER 16. METHODS FOR DRAG DETERMINATION IN FLIGHT 161
16.1 INTRODUCTION 161 16.2 SPEED POWER METHOD 161 16.3 PROP-FEATHERED
SINKS OR GLIDE POLARS 164 16.4 INCREMENTAL DRAG METHOD 166 16.5
INCREMENTAL POWER METHOD 167 REFERENCES 167 CHAPTER 17. AIRSPEED VS
FLIGHT PATH ANGLE PERFORMANCE METHOD FOR POWERED-LIFT AIRCRAFT 169 17.1
INTRODUCTION 169 17.2 V-Y METHOD 169 REFERENCES 1 74 CHAPTER 18. TAKEOFF
AND LANDING THEORY AND METHODS 177 18.1 INTRODUCTION 177 18.2 FEDERAL
AVIATION ADMINISTRATION REGULATIONS 177 18.3 THEORY 180 18.4 TEST
METHODS 184 18.5 TEST PROCEDURES 187 18.6 DATA REDUCTION 188 18.7
REJECTED TAKEOFF DISTANCES 197 REFERENCES 197 PART 2 STABILITY AND
CONTROL FLIGHT TESTING CHAPTER 19. INTRODUCTION TO STABILITY AND CONTROL
FLIGHT TESTING . 201 19.1 INTRODUCTION 201 19.2 REGULATIONS 201 19.3
REFERENCE AXES SYSTEMS 201 19.4 DEFINITIONS OF STABILITY AND
CONTROLLAHILRTV TABLE OF CONTENTS XIII 19.5 RELATION OF STABILITY AND
CONTROL TO THE AIRCRAFT S E.G. ENVELOPE 206 19.6 CONTROL SYSTEM
CHARACTERISTICS 207 REFERENCES 207 CHAPTER 20. STATIC LONGITUDINAL
STABILITY THEORY 209 20.1 INTRODUCTION 209 20.2 STICK-FIXED STATIC
LONGITUDINAL STABILITY 210 20.3 LONGITUDINAL CONTROL 215 20.4 ELEVATOR
POSITION STABILITY 216 20.5 STICK-FREE LONGITUDINAL STABILITY 218 20.6
CONTROL FORCE STABILITY 219 20.7 STICK-FREE LONGITUDINAL STATIC
STABILITY FOR AN IRREVERSIBLE CONTROL SYSTEM 221 REFERENCES 221 CHAPTER
21. STATIC LONGITUDINAL STABILITY FLIGHT TEST METHODS 223 21.1
INTRODUCTION 223 21.2 FEDERAL AVIATION ADMINISTRATION REGULATIONS 223
21.3 STICK-FIXED NEUTRAL POINT DETERMINATION 224 21.4 STICK-FREE NEUTRAL
POINT DETERMINATION 225 21.5 FLIGHT TEST METHOD FOR DETERMINATION OF
NEUTRAL POINTS. . . 230 21.6 OTHER STATIC LONGITUDINAL STABILITY TESTS
230 REFERENCES 233 CHAPTER 22. DYNAMIC LONGITUDINAL STABILITY THEORY 235
22.1 INTRODUCTION 235 22.2 THEORY 236 22.3 LONG PERIOD OR PHUGOID 238
22.4 SHORT PERIOD 240 22.5 ELEVATOR SHORT PERIOD 246 REFERENCES 246
CHAPTER 23. DYNAMIC LONGITUDINAL STABILITY FLIGHT TEST METHODS AND DATA
REDUCTION 247 23.1 INTRODUCTION 247 23.2 FEDERAL AVIATION ADMINISTRATION
REGULATIONS 247 23.3 FLIGHT TEST METHODS FOR EVALUATING THE PHUGOID 248
23.4 PHUGOID DATA REDUCTION 248 23.5 SHORT PERIOD FLIGHT TEST METHODS
249 23.6 SHORT PERIOD DATA REDUCTION 252 REFERENCES 253 XIV TABLE OF
CONTENTS CHAPTER 24. LONGITUDINAL MANEUVERING STABILITY THEORY 255 24.1
INTRODUCTION 255 24.2 ELEVATOR POSITION MANEUVERING STABILITY 257 24.3
STICK-FORCE MANEUVERING STABILITY 259 24.4 COMPRESSIBILITY EFFECTS 264
REFERENCES 264 CHAPTER 25. MANEUVERING STABILITY METHODS AND DATA
REDUCTION 265 25.1 INTRODUCTION 265 25.2 FEDERAL AVIATION ADMINISTRATION
REGULATIONS 265 25.3 EVALUATION BY PILOT OPINION 266 25.4 FLIGHT TEST
METHODS FOR QUANTITATIVE EVALUATION 267 25.5 DATA REDUCTION TECHNIQUES
271 REFERENCES 273 CHAPTER 26. LONGITUDINAL CONTROL AND TRIM THEORY AND
FLIGHT TEST METHODS 275 26.1 INTRODUCTION 275 26.2 FEDERAL AVIATION
ADMINISTRATION REGULATIONS 276 26.3 LONGITUDINAL CONTROL 278 26.4
LONGITUDINAL TRIM 280 REFERENCES 283 CHAPTER 27. METHODS FOR IMPROVING
LONGITUDINAL STABILITY AND CONTROL 285 27.1 INTRODUCTION 285 27.2
CONTROL SYSTEM GADGETS 285 27.3 ELEVATOR TABS 288 27.4 AERODYNAMIC
BALANCE 292 REFERENCES 296 CHAPTER 28. LATERAL-DIRECTIONAL STABILITY
THEORY AND FLIGHT TEST METHODS 297 28.1 INTRODUCTION 297 28.2 FEDERAL
AVIATION ADMINISTRATION REGULATIONS 297 28.3 THEORY 299 28.4 DIRECTIONAL
STABILITY 300 28.5 LATERAL STABILITY 302 28.6 SIDE FORCE 304 28.7
CONTROL-FREE, LATERAL-DIRECTIONAL STABILITY . . 306 28.8 FLIGHT TEST
METHODS 308 REFERENCES 310 TABLE OF CONTENTS XV CHAPTER 29. DYNAMIC
LATERAL-DIRECTIONAL STABILITY THEORY AND FLIGHT TEST METHODS 311 29.1
INTRODUCTION 311 29.2 FEDERAL AVIATION ADMINISTRATION REGULATIONS 311
29.3 THEORY 312 29.4 SPIRAL MODE 314 29.5 ROLL MODE 315 29.6 DUTCH ROLL
MODE 315 29.7 EFFECTS OF LATERAL-DIRECTIONAL PARAMETERS ON
LATERAL-DIRECTIONAL DYNAMICS 316 29.8 FLIGHT TEST METHODS FOR EVALUATING
DYNAMIC LATERAL- DIRECTIONAL STABILITY 320 REFERENCES 322 CHAPTER 30.
LATERAL CONTROL POWER (ROLLING PERFORMANCE) .... 323 30.1 INTRODUCTION
323 30.2 FEDERAL AVIATION ADMINISTRATION REGULATIONS 323 30.3 SINGLE
DEGREE OF FREEDOM ROLL RESPONSE 324 30.4 INFLUENCE OF VARIOUS PARAMETERS
ON ROLLING PERFORMANCE . . 327 30.5 LATERAL CONTROL IN THE REAL CASE 331
30.6 OTHER METHODS OF ROLL CONTROL 340 REFERENCES 340 CHAPTER 31.
DIRECTIONAL CONTROL 341 31.1 INTRODUCTION 341 31.2 FEDERAL AVIATION
ADMINISTRATION REGULATIONS 341 31.3 DIRECTIONAL CONTROL*SINGLE-ENGINE
AIRPLANES 344 31.4 DIRECTIONAL CONTROL*MULTIENGINE AIRPLANES 345 31.5
METHODS FOR DETERMINING C N& 349 REFERENCES 357 CHAPTER 32. FLYING
QUALITIES 359 32.1 INTRODUCTION 359 32.2 FEDERAL AVIATION ADMINISTRATION
REGULATIONS 359 32.3 COOPER-HARPER PILOT RATING SCALE 359 32.4 LEVELS OF
FLYING QUALITIES 361 32.5 FLIGHT TEST PROCEDURES 361 REFERENCES 363 PART
3 HAZARDOUS FLIGHT TESTS CHAPTER 33. STALL CHARACTERISTICS 367 33.1
INTRODUCTION 367 33.2 FEDERAL AVIATION ADMINISTRATION REGULATIONS 367
XVI TABLE OF CONTENTS 33.3 STALL CHARACTERISTICS THEORY 372 33.4
AIRCRAFT LOADING 372 33.5 SAFETY CONSIDERATIONS 372 33.6 FLIGHT TEST
METHOD 373 33.7 DATA REQUIREMENTS 375 33.8 POTENTIAL PROBLEMS 376 33.9
PROBLEM FIXES 377 REFERENCES 381 CHAPTER 34. AIRPLANE SPIN TESTING 383
34.1 INTRODUCTION 383 34.2 FEDERAL AVIATION ADMINISTRATION REGULATIONS
384 34.3 SPIN THEORY 390 34.4 PLANNING FOR SPIN TESTING 405 34.5 FLIGHT
TEST METHOD 409 REFERENCES 415 CHAPTER 35. DIVE TESTING FOR FLUTTER,
VIBRATION, AND BUFFETING 417 35.1 INTRODUCTION 417 35.2 FEDERAL AVIATION
ADMINISTRATION REGULATIONS 417 35.3 THEORY ; 419 35.4 SAFETY
CONSIDERATIONS 422 35.5 INSTRUMENTATION 424 35.6 FLIGHT TEST METHOD ,
424 35.7 DATA ANALYSIS 426 REFERENCES 426
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| indexdate | 2024-07-09T19:13:55Z |
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| isbn | 1563475642 |
| language | English |
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| physical | XVIII, 441 S. Ill., graph. Darst. |
| publishDate | 2003 |
| publishDateSearch | 2003 |
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| publisher | American Institute of Aeronautics and Astronautics |
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| spelling | Kimberlin, Ralph D. Verfasser aut Flight testing of fixed-wing aircraft Ralph D. Kimberlin Reston, VA American Institute of Aeronautics and Astronautics 2003 XVIII, 441 S. Ill., graph. Darst. txt rdacontent n rdamedia nc rdacarrier AIAA education series Includes bibliographical references and index. Avions - Essais en vol Airplanes Flight testing Starrflügelflugzeug (DE-588)4182936-0 gnd rswk-swf Flugerprobung (DE-588)4352769-3 gnd rswk-swf Starrflügelflugzeug (DE-588)4182936-0 s Flugerprobung (DE-588)4352769-3 s DE-604 HEBIS Datenaustausch Darmstadt application/pdf http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=010321430&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA Inhaltsverzeichnis |
| spellingShingle | Kimberlin, Ralph D. Flight testing of fixed-wing aircraft Avions - Essais en vol Airplanes Flight testing Starrflügelflugzeug (DE-588)4182936-0 gnd Flugerprobung (DE-588)4352769-3 gnd |
| subject_GND | (DE-588)4182936-0 (DE-588)4352769-3 |
| title | Flight testing of fixed-wing aircraft |
| title_auth | Flight testing of fixed-wing aircraft |
| title_exact_search | Flight testing of fixed-wing aircraft |
| title_full | Flight testing of fixed-wing aircraft Ralph D. Kimberlin |
| title_fullStr | Flight testing of fixed-wing aircraft Ralph D. Kimberlin |
| title_full_unstemmed | Flight testing of fixed-wing aircraft Ralph D. Kimberlin |
| title_short | Flight testing of fixed-wing aircraft |
| title_sort | flight testing of fixed wing aircraft |
| topic | Avions - Essais en vol Airplanes Flight testing Starrflügelflugzeug (DE-588)4182936-0 gnd Flugerprobung (DE-588)4352769-3 gnd |
| topic_facet | Avions - Essais en vol Airplanes Flight testing Starrflügelflugzeug Flugerprobung |
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