°£Æí°áÁ¦, ½Å¿ëÄ«µå û±¸ÇÒÀÎ
ÀÎÅÍÆÄÅ© ·Ôµ¥Ä«µå 5% (44,650¿ø)
(ÃÖ´ëÇÒÀÎ 10¸¸¿ø / Àü¿ù½ÇÀû 40¸¸¿ø)
ºÏÇǴϾð ·Ôµ¥Ä«µå 30% (32,900¿ø)
(ÃÖ´ëÇÒÀÎ 3¸¸¿ø / 3¸¸¿ø ÀÌ»ó °áÁ¦)
NH¼îÇÎ&ÀÎÅÍÆÄÅ©Ä«µå 20% (37,600¿ø)
(ÃÖ´ëÇÒÀÎ 4¸¸¿ø / 2¸¸¿ø ÀÌ»ó °áÁ¦)
Close

Mechanics of Flight

¼Òµæ°øÁ¦

2013³â 9¿ù 9ÀÏ ÀÌÈÄ ´©Àû¼öÄ¡ÀÔ´Ï´Ù.

°øÀ¯Çϱâ
Á¤°¡

47,000¿ø

  • 47,000¿ø

    1,410P (3%Àû¸³)

ÇÒÀÎÇýÅÃ
Àû¸³ÇýÅÃ
  • S-Point Àû¸³Àº ¸¶ÀÌÆäÀÌÁö¿¡¼­ Á÷Á¢ ±¸¸ÅÈ®Á¤ÇϽŠ°æ¿ì¸¸ Àû¸³ µË´Ï´Ù.
Ãß°¡ÇýÅÃ
¹è¼ÛÁ¤º¸
  • 5/23(¸ñ) À̳» ¹ß¼Û ¿¹Á¤  (¼­¿ï½Ã °­³²±¸ »ï¼º·Î 512)
  • ¹«·á¹è¼Û
ÁÖ¹®¼ö·®
°¨¼Ò Áõ°¡
  • À̺¥Æ®/±âȹÀü

  • ¿¬°üµµ¼­

  • »óÇ°±Ç

AD

¸ñÂ÷

Preface
Acknowledgments
Overview of Aerodynamics
Introduction and Notation
Fluid Statics and the Atmosphere
The Boundary Layer Concept
Inviscid Aerodynamics
Review of Elementary Potential Flows
Incompressible Flow over Airfoils
Trailing-Edge Flaps and Section Flap Effectiveness
Incompressible Flow over Finite Wings
Flow over Multiple Lifting Surfaces
Inviscid Compressible Aerodynamics
Compressible Subsonic Flow
Supersonic Flow
Problems
Overview of Propulsion
Introduction
The Propeller
Propeller Blade Theory
Propeller Momentum Theory
Off-Axis Forces and Moments Developed by a Propeller
Turbojet Engines: The Thrust Equation
Turbojet Engines: Cycle Analysis
The Turbojet Engine with Afterburner
Turbofan Engines
Problems
Aircraft Performance
Introduction
Thrust Required
Power Required
Rate of Climb and Power Available
Fuel Consumption and Endurance
Fuel Consumption and Range
Power Failure and Gliding Flight
Airspeed, Wing Loading, and Stall
The Steady Coordinated Turn
Takeoff and Landing Performance
Accelerating Climb and Balanced Field Length
Problems
Longitudinal Static Stability and Trim
Fundamentals of Static Equilibrium and Stability
Pitch Stability of a Cambered Wing
Simplified Pitch Stability Analysis for a Wing-Tail Combination
Stick-Fixed Neutral Point and Static Margin
Estimating the Downwash Angle on an Aft Tail
Simplified Pitch Stability Analysis for a Wing-Canard Combination
Effects of Drag and Vertical Offset
Contribution of the Fuselage and Nacelles
Contribution of Running Propellers
Contribution of Jet Engines
Problems
Lateral Static Stability and Trim
Introduction
Yaw Stability and Trim
Estimating the Sidewash Gradient on a Vertical Tail
Estimating the Lift Slope for a Vertical Tail
Roll Stability and Dihedral Effect
Roll Control and Trim Requirements
Longitudinal-Lateral Coupling
Control Surface Sign Conventions
Problems
Aircraft Controls and Maneuverability
Longitudinal Control and Maneuverability
Effects of Structural Flexibility
Control Force and Trim Tabs
Stick-Free Neutral and Maneuver Points
Ground Effect, Elevator Sizing, and CG Limits
Stall Recovery
Lateral Control and Maneuverability
Aileron Reversal
Other Control Surface Configurations
Airplane Spin
Problems
Aircraft Equations of Motion
Introduction
Newton's Second Law for Rigid-Body Dynamics
Position and Orientation: The Euler Angle Formulation
Rigid-Body 6-DOF Equations of Motion
Linearized Equations of Motion
Force and Moment Derivatives
Nondimensional Linearized Equations of Motion
Transformation of Stability Axes
Inertial and Gyroscopic Coupling
Problems
Linearized Longitudinal Dynamics
Fundamentals of Dynamics: Eigenproblems
Longitudinal Motion: The Linearized Coupled Equations
Short-Period Approximation
Long-Period Approximation
Pure Pitching Motion
Summary
Problems
Linearized Lateral Dynamics
Introduction
Lateral Motion: The Linearized Coupled Equations
Roll Approximation
Spiral Approximation
Dutch Roll Approximation
Table of Contents provided by Publisher. All Rights Reserved.

Ã¥¼Ò°³

Mechanics of Flight is a unique combination of theory and applications organized in a logical presentation. It affords readers extensive coverage of individual topics within flight mechanics, including overviews of aerodynamics and propulsion. It also offers a full range of modern and classical techniques for applying fundamental principles to the solution of engineering problems in fight mechanics. Mechanics of Flight explores the basic principles of flight mechanics with the help of many worked examples, starting with simple problems involving steady-level flight and building to more complex ones such as the analysis of turning flight and spins. Special coverage found here-and not in most books on the subject-includes a detailed presentation of the quaternion formulation for six-degree-of-freedom flight simulation, including treatment of efficient numerical integration methods.

ÀúÀÚ¼Ò°³

Phillips, Warren F. [Àú] ½ÅÀ۾˸² SMS½Åû
»ý³â¿ùÀÏ -

ÇØ´çÀÛ°¡¿¡ ´ëÇÑ ¼Ò°³°¡ ¾ø½À´Ï´Ù.

ÄÄÇ»ÅÍ ºÐ¾ß¿¡¼­ ¸¹Àº ȸ¿øÀÌ ±¸¸ÅÇÑ Ã¥

    ¸®ºä

    0.0 (ÃÑ 0°Ç)

    100ÀÚÆò

    ÀÛ¼º½Ã À¯ÀÇ»çÇ×

    ÆòÁ¡
    0/100ÀÚ
    µî·ÏÇϱâ

    100ÀÚÆò

    0.0
    (ÃÑ 0°Ç)

    ÆǸÅÀÚÁ¤º¸

    • ÀÎÅÍÆÄÅ©µµ¼­¿¡ µî·ÏµÈ ¿ÀǸ¶ÄÏ »óÇ°Àº ±× ³»¿ë°ú Ã¥ÀÓÀÌ ¸ðµÎ ÆǸÅÀÚ¿¡°Ô ÀÖÀ¸¸ç, ÀÎÅÍÆÄÅ©µµ¼­´Â ÇØ´ç »óÇ°°ú ³»¿ë¿¡ ´ëÇØ Ã¥ÀÓÁöÁö ¾Ê½À´Ï´Ù.

    »óÈ£

    (ÁÖ)±³º¸¹®°í

    ´ëÇ¥ÀÚ¸í

    ¾Èº´Çö

    »ç¾÷ÀÚµî·Ï¹øÈ£

    102-81-11670

    ¿¬¶ôó

    1544-1900

    ÀüÀÚ¿ìÆíÁÖ¼Ò

    callcenter@kyobobook.co.kr

    Åë½ÅÆǸž÷½Å°í¹øÈ£

    01-0653

    ¿µ¾÷¼ÒÀçÁö

    ¼­¿ïƯº°½Ã Á¾·Î±¸ Á¾·Î 1(Á¾·Î1°¡,±³º¸ºôµù)

    ±³È¯/ȯºÒ

    ¹ÝÇ°/±³È¯ ¹æ¹ý

    ¡®¸¶ÀÌÆäÀÌÁö > Ãë¼Ò/¹ÝÇ°/±³È¯/ȯºÒ¡¯ ¿¡¼­ ½Åû ¶Ç´Â 1:1 ¹®ÀÇ °Ô½ÃÆÇ ¹× °í°´¼¾ÅÍ(1577-2555)¿¡¼­ ½Åû °¡´É

    ¹ÝÇ°/±³È¯°¡´É ±â°£

    º¯½É ¹ÝÇ°ÀÇ °æ¿ì Ãâ°í¿Ï·á ÈÄ 6ÀÏ(¿µ¾÷ÀÏ ±âÁØ) À̳»±îÁö¸¸ °¡´É
    ´Ü, »óÇ°ÀÇ °áÇÔ ¹× °è¾à³»¿ë°ú ´Ù¸¦ °æ¿ì ¹®Á¦Á¡ ¹ß°ß ÈÄ 30ÀÏ À̳»

    ¹ÝÇ°/±³È¯ ºñ¿ë

    º¯½É ȤÀº ±¸¸ÅÂø¿À·Î ÀÎÇÑ ¹ÝÇ°/±³È¯Àº ¹Ý¼Û·á °í°´ ºÎ´ã
    »óÇ°À̳ª ¼­ºñ½º ÀÚüÀÇ ÇÏÀÚ·Î ÀÎÇÑ ±³È¯/¹ÝÇ°Àº ¹Ý¼Û·á ÆǸÅÀÚ ºÎ´ã

    ¹ÝÇ°/±³È¯ ºÒ°¡ »çÀ¯

    ·¼ÒºñÀÚÀÇ Ã¥ÀÓ ÀÖ´Â »çÀ¯·Î »óÇ° µîÀÌ ¼Õ½Ç ¶Ç´Â ÈÑ¼ÕµÈ °æ¿ì
    (´ÜÁö È®ÀÎÀ» À§ÇÑ Æ÷Àå ÈѼÕÀº Á¦¿Ü)

    ·¼ÒºñÀÚÀÇ »ç¿ë, Æ÷Àå °³ºÀ¿¡ ÀÇÇØ »óÇ° µîÀÇ °¡Ä¡°¡ ÇöÀúÈ÷ °¨¼ÒÇÑ °æ¿ì
    ¿¹) È­ÀåÇ°, ½ÄÇ°, °¡ÀüÁ¦Ç°(¾Ç¼¼¼­¸® Æ÷ÇÔ) µî

    ·º¹Á¦°¡ °¡´ÉÇÑ »óÇ° µîÀÇ Æ÷ÀåÀ» ÈѼÕÇÑ °æ¿ì
    ¿¹) À½¹Ý/DVD/ºñµð¿À, ¼ÒÇÁÆ®¿þ¾î, ¸¸È­Ã¥, ÀâÁö, ¿µ»ó È­º¸Áý

    ·½Ã°£ÀÇ °æ°ú¿¡ ÀÇÇØ ÀçÆǸŰ¡ °ï¶õÇÑ Á¤µµ·Î °¡Ä¡°¡ ÇöÀúÈ÷ °¨¼ÒÇÑ °æ¿ì

    ·ÀüÀÚ»ó°Å·¡ µî¿¡¼­ÀÇ ¼ÒºñÀÚº¸È£¿¡ °üÇÑ ¹ý·üÀÌ Á¤ÇÏ´Â ¼ÒºñÀÚ Ã»¾àöȸ Á¦ÇÑ ³»¿ë¿¡ ÇØ´çµÇ´Â °æ¿ì

    »óÇ° Ç°Àý

    °ø±Þ»ç(ÃâÆÇ»ç) Àç°í »çÁ¤¿¡ ÀÇÇØ Ç°Àý/Áö¿¬µÉ ¼ö ÀÖÀ½

    ¼ÒºñÀÚ ÇÇÇغ¸»ó
    ȯºÒÁö¿¬¿¡ µû¸¥ ¹è»ó

    ·»óÇ°ÀÇ ºÒ·®¿¡ ÀÇÇÑ ±³È¯, A/S, ȯºÒ, Ç°Áúº¸Áõ ¹× ÇÇÇغ¸»ó µî¿¡ °üÇÑ »çÇ×Àº ¼ÒºñÀÚºÐÀïÇØ°á ±âÁØ (°øÁ¤°Å·¡À§¿øȸ °í½Ã)¿¡ ÁØÇÏ¿© 󸮵Ê

    ·´ë±Ý ȯºÒ ¹× ȯºÒÁö¿¬¿¡ µû¸¥ ¹è»ó±Ý Áö±Þ Á¶°Ç, ÀýÂ÷ µîÀº ÀüÀÚ»ó°Å·¡ µî¿¡¼­ÀÇ ¼ÒºñÀÚ º¸È£¿¡ °üÇÑ ¹ý·ü¿¡ µû¶ó ó¸®ÇÔ

    (ÁÖ)KGÀ̴Ͻýº ±¸¸Å¾ÈÀü¼­ºñ½º¼­ºñ½º °¡ÀÔ»ç½Ç È®ÀÎ

    (ÁÖ)ÀÎÅÍÆÄÅ©Ä¿¸Ó½º´Â ȸ¿ø´ÔµéÀÇ ¾ÈÀü°Å·¡¸¦ À§ÇØ ±¸¸Å±Ý¾×, °áÁ¦¼ö´Ü¿¡ »ó°ü¾øÀÌ (ÁÖ)ÀÎÅÍÆÄÅ©Ä¿¸Ó½º¸¦ ÅëÇÑ ¸ðµç °Å·¡¿¡ ´ëÇÏ¿©
    (ÁÖ)KGÀ̴Ͻýº°¡ Á¦°øÇÏ´Â ±¸¸Å¾ÈÀü¼­ºñ½º¸¦ Àû¿ëÇÏ°í ÀÖ½À´Ï´Ù.

    ¹è¼Û¾È³»

    • ±³º¸¹®°í »óÇ°Àº Åùè·Î ¹è¼ÛµÇ¸ç, Ãâ°í¿Ï·á 1~2Àϳ» »óÇ°À» ¹Þ¾Æ º¸½Ç ¼ö ÀÖ½À´Ï´Ù.

    • Ãâ°í°¡´É ½Ã°£ÀÌ ¼­·Î ´Ù¸¥ »óÇ°À» ÇÔ²² ÁÖ¹®ÇÒ °æ¿ì Ãâ°í°¡´É ½Ã°£ÀÌ °¡Àå ±ä »óÇ°À» ±âÁØÀ¸·Î ¹è¼ÛµË´Ï´Ù.

    • ±ººÎ´ë, ±³µµ¼Ò µî ƯÁ¤±â°üÀº ¿ìü±¹ Åù踸 ¹è¼Û°¡´ÉÇÕ´Ï´Ù.

    • ¹è¼Ûºñ´Â ¾÷ü ¹è¼Ûºñ Á¤Ã¥¿¡ µû¸¨´Ï´Ù.

    • - µµ¼­ ±¸¸Å ½Ã 15,000¿ø ÀÌ»ó ¹«·á¹è¼Û, 15,000¿ø ¹Ì¸¸ 2,500¿ø - »óÇ°º° ¹è¼Ûºñ°¡ ÀÖ´Â °æ¿ì, »óÇ°º° ¹è¼Ûºñ Á¤Ã¥ Àû¿ë