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DATCOMの目次とページ数一覧

USAF Stability and Control DATCOMの3134ページある化け物PDFの目次とページ数の一覧

References for the Digtal Datcom Program
A list of references for Digital Datcom
ChapterTitlePage
1GUIDE TO DATCOM and METHODS SUMMARY15
2GENERAL INFORMATION
- 2.1General Notation131
- 2.2Wing227
- - 2.2.1section parameters
- - 2.2.2PLANFORM PARAMETERS235
- 2.3Body Parameters240
3EFFECTS OF EXTERNAL STORES245
- 3.1Effect of External Stores on Aircraft Lift260
- - 3.1.1Increment Due to Store Installations262
- - 3.1.2Lift Increment Due Installations288
- - 3.1.3Total Lift Inclement to External Stores296
- 3.2Effect of External Stores tm Aircraft Drag301
- - 3.2.1Drag Zero Lift303
- - - 3.2.1.1Basic Drag Due to Store Installations
- - - 3.2.1.2Drag Due to Adjacent Store Interference362
- - - 3.2.1.3Drag Due to Fuselage Interference368
- - 3.2.2Drag Dug to Lift371
- - 3.2.3Total Drag Increment Due to External Stores374
- 3.3Effect of External Stores on Aircraft Neutral Point379
- - 3.3.1Neutral-point Shift Due Lift Transfer from Store Installation Clean Aircraf380
- - 3.3.2Neutral-Point Shift Due to Interference Effects on Wing Flow Field411
- - 3.3.3Neutral-Point Shift Due to in Effectiveness423
- - 3.3.4To Neutral-point Shift Due to External Stores429
- 3.4Effect of Stores Aircraft Side431
- 3.5Effect Of External Stores on Aircraft Y awing Moment448
- 3.6Effect of External Stores on Aircraft Rolling Moment460
4CHARACTERISTICS AT ANGLE OF ATTACK461
- 4.1Wings at Angle of Attack
- - 4.1.1SECTION LIFT
- - - 4.1.1.1Section Zero-Lift of Attack468
- - - 4.1.1.2Section Lift-Curve Slope471
- - - 4.1.1.3Section Lift Variation with Angle of Attack Near Maximum Lift479
- - - 4.1.1.4Section Maximum Lift481
- - 4.1.2Pitching Moment489
- - - 4.1.2.1Section Zero Lift Pitching Moment
- - - 4.1.2.2Section Pitching-Moment Variation with Lift490
- - 4.1.3Wing Lift494
- - - 4.1.3.1Wing Zero Lift Ange of Attack496
- - - 4.1.3.2Wing Lift-curve Slope501
- - - 4.1.3.3Wins Lift in the Ange of Attack566
- - - 4.1.3.4Wing Maximum Lift625
- - 4.1.4Wing Pitching Moment652
- - - 4.1.4.1Wing Pitching Moment654
- - - 4.1.4.2Wing Pitching Moment Curve Slope662
- - - 4.1.4.3Wing Pitching Moment in the Angle-of-Attack695
- - 4.1.5Wing Drag722
- - - 4.1.5.1Wing Zero-Lift Drag
- - - 4.1.5.2Wing Drag at Angle of Attack756
- 4.2Bodies at Angle of Attack815
- - 4.2.1Body Lift
- - - 4.2.1.1Body Lift Curve Slope
- - - 4.2.1.2Body Lift in the A Range841
- - 4.2.2Body Pitching Moment885
- - - 4.2.2.1Body Pitching-Moment-Curve Slope
- - - 4.2.2.2Body pitching Moment in the Nonlinear Angle-of-Attack Range912
- - 4.2.3Body Drag939
- - - 4.2.3.1Body Zero-Lift Drag
- - - 4.2.3.2Body Drag at of Attack1008
- 4.3Wing-Body Tail-Body Combinations at Angle of Attack1036
- - 4.3.1Wing-Body Lift1036
- - - 4.3.1.1
- - - 4.3.1.2Wing-Body Lift Curve Slope
- - - 4.3.1.3Wing-Body Lift in the Nonlinear Angle of Attack1048
- - - 4.3.1.4Wing-Body Lift1063
- - 4.3.2Wing-Body Pitching Moment1075
- - - 4.3.2.1Wing-Body Pitching Moment
- - - 4.3.2.2Wing-Body Pitching Moment Curve Slope1091
- - 4.3.3Wing-Body Drag1128
- - - 4.3.3.1Wing-Body Zero-Lin Drag
- - - 4.3.3.2Wing-Body Drag at Angle of Attack1167
- 4.4Wing-Wing Combinations at Angle of Attack (Wing Fields)1203
- - 4.4.1Wing-Wing Combinations at Angle of Attack (その2)
- 4.5Wing-Body-Tail Combinations at Angle of Attack1286
- - 4.5.1Wing-Body-Tail Lift
- - - 4.5.1.1Wing-Body-Tail Lift curve Slope
- - - 4.5.1.2Wing-Body-Tail Lift in Angle of Attack1294
- - - 4.5.1.3Wing-Body-Tail Maximum Lift1314
- - 4.5.2Wing-Body-Tail Pitching Moment1318
- - - 4.5.2.1Wing-Body-Tail Pitching Moment Curve Slope
- - 4.5.3Wing-Body-Tail Drag1326
- - - 4.5.3.1Wing-Body-Tail Zero Lift Drag
- - - 4.5.3.2Wing-Body-Tail Drag at Angle or Attack1345
- 4.6Power Effect at Angle of Attack1350
- - 4.6.1Power Effects on Lift Variation with Angle of Attack1363
- - 4.6.2Power Effects on lift1396
- - 4.6.3Power Effects on Pitching-Moment Variation with Angle of Attack1399
- - 4.6.4Power Effects on Drag at Angle of Attack1412
- 4.7Ground Effects at Angle of Attack1433
- - 4.7.1Ground Effects on Lift Variation with Angle of Attack1442
- - 4.7.3Ground Effects on Pitching-Moment Variation with Angle of Attack1464
- - 4.7.4Ground Effects on Drag at Angle of Attack1467
- 4.8Low-Aspect-Ratio Wings and Wing-Body Combinations at Angle of Attack1472
- - 4.8.1Wing, Wing-Body Normal Force1484
- - - 4.8.1.1Wing, Wing-Body Zero Normal-Force Angle of Attack
- - - 4.8.1.2Wing, Wing-Body Normal-Force Variation with Angle of Attack1488
- - 4.8.2Wing-Body Axial Force1502
- - - 4.8.2.1Wing, Wing-Body Zero-Normal-Foree Axial Force
- - - 4.8.2.2Wing, Wing-Body Axial-Force Variation with Angle of Attack1509
- - 4.8.3Wing, Wing-Body Pitching Moment1520
- - - 4.8.3.1Wing, Wing-Body Zero Normal-Force Pitching Moment
- - - 4.8.3.2Wing, Wing-Body Pitching-Moment Variation with Angle of Attack1524
5CHARACTERISTICS IN SIDESLIP1531
- 5.1Wings in Sideslip
- - 5.1.1Wing Sideslip Derivative Cyb
- - - 5.1.1.1Wing Sideslip Derivative Cyb in the Linear Angle-of-Attack Range
- - 5.1.2Wing Sideslip Derivative Clb1537
- - - 5.1.2.1Wing Sideslip Derivative Clb in the Linear Angle-of-Attack Range
- - - 5.1.2.2Wing Rolling-Moment Coefficient CI at Angle of Attack1570
- - 5.1.3Wing Sideslip Derivative Cnb1576
- - - 5.1.3.1Wing Sideslip Derivative Cnb in the Linear Angle-of-Attack Range
- 5.2Wing-Body Combinations in Sideslip1582
- - 5.2.1Wing-Body Sideslip Derivative Cy
- - - 5.2.1.1Wing-Body Sideslip Derivative Cyb in the Linear Angle-of-Attack Range
- - - 5.2.1.2Wing-Body Side-Force Coefficient Cy at Angle of Attack1589
- - 5.2.2Wing-Body Sideslip Derivative Clb1600
- - - 5.2.2.1Wing-Body Sideslip Derivative CIb in the Linear Angle-of-Attack Range
- - 5.2.3Wing-Body Sideslip Derivative Cnb1626
- - - 5.2.3.1Wing-Body Sideslip Derivative Cnb in the Linear Angle-of-Attack Range
- - - 5.2.3.2Wing-Body Yawing-Mome nt Coefficient Cn at Angle of Attack1635
- 5.3Tail-Body Combinations in Sideslip1643
- - 5.3.1Tail-Body Sideslip Derivative Cyb
- - - 5.3.1.1Tail-Body Sideslip Derivative Cyb in the Linear Angle-of-Attack Range
- - - 5.3.1.2Tail-Rody Side-Force Coefficient Cyb at Angle of Attack1711
- - 5.3.2Tail-Body Sideslip Derivative CIb1726
- - - 5.3.2.1Tail-Body Sideslip Derivative Clb in the Linear Angle-of-Attack Range
- - 5.3.3Tail-Body Sideslip Derivative Cnb1739
- - - 5.3.3.1Tail-Body Sideslip Derivative Cnb in the Linear Angle-of-Attack Range
- - - 5.3.3.2Tail-Body Yawing-Moment Coefficient Cn at Angle of Attack1750
- 5.4Flow Fields in Sideslip1754
- - 5.4.1Wing-Body Wake and Sidewash in Sideslip
- 5.5Low-Aspect-Ratio Wings and Wing-Body Combinations in Sideslip1758
- - 5.5.1Wing, Wing-Body Sideslip Derivative Kyb1764
- - - 5.5.1.1Wing, Wing-Body Sideslip Derivative Kyb at Zero Normal Force
- - - 5.5.1.2Wing, Wing-Body Sideslip Derivative Kyb Variation with Angle of Attack1770
- - 5.5.2Wing, Wing-Body Sideslip Derivative1779
- - - 5.5.2.1Wing, Wing-Body Sideslip Derivative KIb Near Zero Normal Force
- - - 5.5.2.2Wing, Wing-Body Sideslip Derivative KIb Variation with Angle of Attack1787
- - 5.5.3Wing, Wing-Body Sideslip Derivative Knb1800
- - - 5.5.3.1Wing, Wing-Body Sideslip Derivative Knb at Zero Normal Force
- - - 5.5.3.2Wing, Wing-Body Sideslip Derivative Variation with Angie of Attack1806
- 5.6Wing-Body-Tail Combinations in Sideslip1812
- - 5.6.1Wing-Body-Tail Sideslip Derivative Cy
- - - 5.6.1.1Wing-Body-Tail Sideslip Derivative Cyb in the Linear Angle-of-Attack Range
- - - 5.6.1.2Wing-Body-Tail Side-Fore Coefficient Cy at Angle of Attack1826
- - 5.6.2Wing-Body-Tail Sideslip Derivative Clb1843
- - - 5.6.2.1Wing-Body-Tail Sideslip Derivative Clb in the Linear
- - 5.6.3Wing-Body-Tail Sideslip Derivative Cnb1858
- - - 5.6.3.1Wing-Body-Tail Sideslip Derivative Cnb in the Linear Angle-of-Attack Range
- - - 5.6.3.2Wing-Body-Tail Yawing-Moment Coefficient at Angle of Attack1866
6CHARACTERISTICS OF HIGH-LIFT AND CONTROL DEVICES1870
- 6.1Symmetrically Deflected Flaps and Control Devices on Wing-Body and Tail-Body
- - 6.1.1Section Lift with High-Lift and Control Devices
- - - 6.1.1.1Section Lift of High-Lift and Control Devices1871
- - - 6.1.1.2Section Lift-Curve Slope with High-Lift and Control Devices1923
- - - 6.1.1.3Section Maximum Lift with High-Lift and Control Devices1929
- - 6.1.2Section Pitching Moment with High-Lift and Control Devices1945
- - - 6.1.2.1Section Pitching-Moment Increment Arm Due to High-Lift and Control Devices
- - - 6.1.2.2Section Derivative cru with High-Lift and Control Devices1982
- - - 6.1.2.3Section Pitching Moment Due to High-Lift and Control Devices Near Maximum L1984
- - 6.1.3Section Hinge Moment of High-Lift and Control Devices1987
- - - 6.1.3.1Section Hinge-Moment Derivative of High-Lift and Control Devices1989
- - - 6.1.3.2Section Hinge-Moment Derivative Ch8 of High-Lift and Devices2002
- - - 6.1.3.3Section Hinge-Moment Derivative (Chi 6t ) of Control Surface Due to Control Ta2015
- - - 6.1.3.4Section Hinge-Moment Derivative (Cht) 5f of Control Tab Due to Control Surface2021
- - 6.1.4Wing Lift with High-Lift and Control Devices2027
- - - 6.1.4.1Control Derivative CLdelta of High-Lift and Control Deuces
- - - 6.1.4.2Wing Lift-Curve Slope with High-Lift and Control Devices2052
- - - 6.1.4.3Wing Maximum Efi with High-Lift and Control Devices2061
- - 6.1.5Wing Pitching Moment with High-Lift and Control Devices2073
- - - 6.1.5.1Pitching-Moment Increment AC.m Due to High-Lift and Control Devices2075
- - - 6.1.5.2Wing Derivative Cm a with High-Lift and Control Devices2148
- - 6.1.6Hinge Moments of High-Lift and Control Devices2149
- - - 6.1.6.1Hinge-Moment Derivative Cha of High-Lift and Control Devices2150
- - - 6.1.6.2Hin$-Moment Derivative Ch(a dot) of High-Lift and Control Devices2189
- - 6.1.7Drag of High-Lift and Control Devices2208
- 6.2Asymmetrically Deflected Controls on Wing-Body and Tail-Body Combinations2236
- - 6.2.1Ro g Moment Due to Asymmetric Deflection of Control Devices
- - - 6.2.1.1Rolling Moment Due to Control Deflection
- - - 6.2.1.2Rolling Moment Due toa Differentially Deflected Horizontal Stabilizer2268
- - 6.2.2Yawing Moment Due to Asymmetric Deflection of Control Devices2292
- - - 6.2.2.1Yawing Moment Due to Control Deflection
- - 6.2.3Side Force Duc to Asymmetric Deflection of Control Devices2309
- 6.3Special Control Methods2310
- - 6.3.1Aerodynamic Control Effectiveness at Hypersonic Speeds
- - 6.3.2Transverse-Jet Control Effectiveness2381
- - 6.3.4Aerodynamically Boosted Control-Surface Tabs2424
7DYNAMIC DERIVATIVES2446
- 7.1Wing Dynamic Derivatives2468
- - 7.1.1Wing Pitching Derivatives2470
- - - 7.1.1.1Wing Pitching Derivative CLq2470
- - - 7.1.1.2Wing Pitching Derivative Cmq2488
- - - 7.1.1.3Wing Pitching Derivative CDq2504
- - 7.1.2Wing Rolling Derivatives2521
- - - 7.1.2.1Wing Rolling Derivative Cyp
- - - 7.1.2.2Wing Rolling Derivative CIp2531
- - - 7.1.2.3Wing Rolling Derivative Cnp2558
- - 7.1.3Wing Yawing Derivatives2578
- - - 7.1.3.1Wing Yawing Derivative Cyr
- - - 7.1.3.2Wing Yawing Derivative CIr2580
- - - 7.1.3.3Wing Yawing Derivative Cnr2592
- - 7.1.4Wing Acceleration Derivatives2599
- - - 7.1.4.1Wing Acceleration Derivative CL(adot)
- - - 7.1.4.2Wing Acceleration Derivative Cm(adot)2617
- - - 7.1.4.3Wing Derivative CDä2637
- 7.2Body Dynamic Derivatives2643
- - 7.2.1Body Pitching Derivatives2646
- - - 7.2.1.1Body Pitching Derivative CLq
- - - 7.2.1.2Body Pitching Derivative Cmq2655
- - 7.2.2Body Acceleration Derivatives2668
- - - 7.2.2.1Body Acceleration Derivative CI(adot)
- - - 7.2.2.2Body Acceleration Derivative Cm(adot)2672
- 7.3Wing-Body Dynamic Derivatives2676
- - 7.3.1Wing-Body Pitching Derivatives
- - - 7.3.1.1Wing-Body Pitching Derivative CLq
- - - 7.3.1.2Wing-Body Pitching Derivative Cmq2686
- - 7.3.2Wing-Body Rolling Derivatives2696
- - - 7.3.2.1Wing-Body Rolling Derivative Cyp
- - - 7.3.2.2Wing-Body Rolling Derivative Clp2698
- - - 7.3.2.3Wing-Body Rolling Derivative Cnp2711
- - 7.3.3Wing-Body Yawing Derivatives2713
- - - 7.3.3.1Wing-Body Yawing Derivative Cyr
- - - 7.3.3.2Wing-Body Yawing Derivative CIr2714
- - - 7.3.3.3Wing-Body Yawing Derivative Cnr2715
- - 7.3.4Wing-Body Acceleration Derivatives2717
- - - 7.3.4.1Wing-Body Acceleration Derivative CL(adot)
- - - 7.3.4.2Wing-Body Acceleration Derivative Cm(adot)2723
- 7.4Wing-Body-Tail Dynamic Derivatives2730
- - 7.4.1Wing-body-Tail Pitching Derivatives
- - - 7.4.1.1Wing-Body-Tail Pitching Derivative CLq
- - - 7.4.1.2Wing-Body-Tail Pitching Derivative Cmq2743
- - - 7.4.1.3Wing-Body-Tail Pitching Derivative CDq2748
- - 7.4.2Wing-Body-Tail Rolling Derivatives2775
- - - 7.4.2.1Wing-Body-Tail Rolling Der ivative Cyp
- - - 7.4.2.2Wing-Body-Tail Rolling Derivative CIp2782
- - - 7.4.2.3Wing-Body-Tail Rolling Derivative Cn p2792
- - 7.4.3Wing-Body-Tail Yawing Derivatives
- - - 7.4.3.1Wing-Body-Tail Yawing Derivative Cyr2799
- - - 7.4.3.2Wing-Body-Tail Yawng Derivative CIr2802
- - - 7.4.3.3Wing-Body-Tail Yawing Derivative Cnr2805
- - 7.4.4Wing-Body-Tail Acceleration Derivatives2808
- - - 7.4.4.1Wing-Body-Tail Acceler ation Derivative
- - - 7.4.4.2Wing-Body-Tail Acceleration Denvative Cm(a dot)2817
- - - 7.4.4.3Wing-Body-Tail Derivative CD(a dot)2822
- - - 7.4.4.4Wing-Body-Tail Derivative Cy(bdot)2825
- - - 7.4.4.5Wing-Body-Tail Derivative Cl(bdot)2886
- - - 7.4.4.6Wing-Body-Tail Derivative Cn(bdot)2888
8MASS AND INERTIA2890
- 8.1Aircraft Mass and Inertia
- 8.2Missile Mass and lnertia2917
9CHARACTERISTICS OF VTOL-STO L AIRCRAFT2928
- 9.1Free Propeller Characteristics3006
- - 9.1.1Propeller Thrust Variation with Angle of Attack3010
- - 9.1.2Propeller Pitching-Moment Variation with Power and Angle of Attack3025
- - 9.1.3Propeller Normal-Force Variation with Power and Angle of Attack3029
- 9.2Propeller-Wing Characteristics3044
- - 9.2.1Propeller-Wing-Flap Lift Variation with Power and Angle of Attack3060
- - 9.2.2Propeller-Wing-Flap Pitching-Moment Variation with Power and Angie of Attack
- - 9.2.3Propeller-Wing-Flap Drag Variation with Power and Angle of Attack3079
- 9.3Ducted-Propeller Characteristics3092
- - 9.3.1Ducted-Propeller Lift Variation with Power and Angle of Attack3111
- - 9.3.2Ducted-Propeller Pitching-Moment Variation with Power and Angle of Attack3125
- - 9.3.3Ducted-Propeller Drag Variation with Power and Angle of Attack3131
DATCOM
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