曝光台 注意防骗
网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
15,200.00 216.65 11,670.80 0.1877 295.07 0.753227E-04
15,400.00 216.65 11,308.48 0.1818 295.07 0.777241E-04
15,600.00 216.65 10,957.40 0.1762 295.07 0.802020E-04
15,800.00 216.65 10,617.22 0.1707 295.07 0.827592E-04
16,000.00 216.65 10,287.60 0.1654 295.07 0.853973E-04
16,200,00 216.65 9,968.22 0.1603 295.07 0.881190E-04
16,400.00 216.65 9,658.75 0.1553 295.07 0.909281E-04
16,600.00 216.65 9,358.89 0.1505 295.07 0.938264E-04
16,800.00 216.65 9,068.34 0.1458 295.07 0.968160E-04
17,000.00 216.65 8,786.81 0.1413 295.07 0.999006E-04
17,200.00 216.65 8,514.02 0.1369 295.07 0.103085E-03
17,400.00 216.65 8,249.70 0.1327 295.07 0.106370E-03
17,600.00 216.65 7,993.59 0.1285 295.07 0.109757E-03
17,800.00 216.65 7,745.42 0.1245 295.07 0.113252E-03
18,000.00 216.65 7,504.96 0.1207 295.07 0.116860E~03
18,200.00 216.65 7,271.97 0.1169 295.07 0.120584E-03
18,400.00 216.65 7,046.20 0.1133 295.07 0.124426E-03
18,600.00 216.65 6,827.45 0.1098 295.07 0.128390E-03
18,800.00 216.65 6,6L5.49 0.1064 295.07 0.132478E-03
19,000.00 216.65 6,410.11 0.1031 295.07 0.136694E-03
~:- -r-=:== -=-__~__________.___, ____:_
Ref: U.S. StandardAtmosphere: /976, National Oceanic and Atmospheric Administration, NASA, and
U.S. Air Force, Washington, DC, 1976.
Bibliography
Anderson, J. D.,lnuoduction to Flight, McGraw-Hill, New York: 1989.
Babister, A. W., Aircrajt Stability and ConU;ol, Pergamon, New York, 1961.
Blakelock, R. C., Automatic Control of Aircra[t and Missiles, Wiley, New York, 1965.
Dickmson, B.,Arrcraft Stability and Control for Pilots and Engrneers, Sir Isaac Pitman and
Sons, London, 1968.
Etkin, B., Dynamics of Flight, Wiley, New York, 1959.
Gerlach, O. H., Lecture Notes on StabiLity and ControL, Parts 1 and 2, Dept. of Aerospace
Engineering, Delft Univ., Delfi, Netherlands, 1983.
Hale, F. J., Aircraft Perj'omumce, Selection, and Design, Wiley, New York, 1984.
McCormick, B. W.,Aerodynanucs, Aeronautics, and Flight Mec/umics, Wiley, New York,
1979.
McRuer, D.,Askenas, I.,and Graham, D.,Aircraft Dynamics and Automatic Control, Prince~
ton Univ., Princeton, NJ, 1973.
Miele, A., Flight Mechanics, VoL 1, 7heo,y of Flight Paths, Addison-Wesley, Reading, MA,
1962.
Nelson, R. C., Flight Stabiluy and Automatic Control, McGraw-Hill, New York, 1989.
Perkins, C. D., and Hage, R. E.,Airplane Perlormance, Stability and Control, l Oth PrinOng,
Wiley, New York, 1965.
Raymer, D. P.,Aircraft D8sign: A ConceptzraL Approach, AIAA Education Series, AIAA,
Washington, DC, 1992.
Roskam, J., Airplane Flight Dynamics and Automatic Flight Control, Part I, Roskam Avi-
ation and Engineering, Lawrence, KS, 1979.
757
A
Abbott, I, H., 177-178
aborted takeoff, 150-151
absolute ceiling, 87-89, 99-100
acceleration, 100-104, 398-403
accidents, causes, 157, 646
aauated forebody strakes, 739~743
adverse yaw, 281, 283, 732
aerodynanuc balancing, 219-224, 286-287
aerodynamic center, 59 .
overview, 19-21
pfessure cemer and, 21-22
wings and, 173-174, 189-191
aerodynamic forces and moments, 376-384
aeroelastic divergence, 56-57
aft upsweep, 171-172
AFTI/F-III aircraft, 677
ailerons, 52, 304, 309, 588-591, 663-664
Air Force B- 1, 50, 60, 106
Airbus 320, 106
airCfaft
class;ification, 593
general turning flight of, 136-138
tailless, 307, 749
see also spectjic aircraft
airfoils
definition, I2
flow over, 41-44
fluid velocity and, 2-3
geometry of, 12-14
Mach numbers and, 40-45
NACA types, 15
pressure distribution over, J 7-18
shapes, 14
supercritical, 45-47
thin, 45
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：
PERFORMANCE, STABILITY, DYNAMICS, AND CONTROL4(108)
