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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,
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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
　
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