[8]Howe, D. Aircraft Conceptual Design Synthesis. Professional Engineering Ltd.; London; 2000.

[9]Raymer, D. Aircraft Design: A Conceptual Approach, 4th edition. AIAA; Reston, VA; 2006.

[10]Kundu, A. K. A Multidisciplinary Study of Aerodynamic Smoothness Requirements Based on V2500 Turbofan Nacelle Data to Reduce Operating Cost. Ph.D. Thesis; October 1999.

CHAPTER 9. AIRCRAFT DRAG

[1]Hoerner, S. F. Fluid Dynamic Drag. DARcorporation; Lawrence, KS; 1965.

[2]AGARD LS 67: Prediction Method for Aircraft Aerodynamic Characteristics; May 1974.

[3]Feagan, R. C., and Morrision, W. D. “Delta Method: An Empirical Drag Buildup Technique.” Lockheed California Company; NASA Contractor Report 151971; 1978.

[4]USAF DATCOM.

[5]ESDU.

[6]Roskam, J. Airplane Design. DARcorporation; Lawrence, KS; 2007.

[7]Kundu, A. K. Subsonic Aircraft Drag Estimation. Shorts Document No. AR/0001 (not in public domain); October 1995.

[8]AGARD AR 256. Technical Status Review on Drag Prediction and Analysis from Computational Fluid Dynamics: State of the Art. June 1989.

[9]Torenbeek, E. Synthesis of Subsonic Airplane Design. Delft University Press; Amsterdam, the Netherlands; 1982.

[10]Haines, A. B. “Subsonic Aircraft Drag: An Appreciation of Present Standards.” Aeronautical Journal; Vol. 72, No. 687; March 1968.

[11]Aircraft Drag Estimation, Cranfield University Notes; 1983.

[11]Young, A. D., and Paterson, J. H. AGARD AG 264. Aircraft Excrescence Drag; 1981.

[12]Kundu, A. K., Watterson, J., et al. “Parametric Optimization of Manufacturing Tolerances at the Aircraft Surface.” Journal of Aircraft, Vol. 39, No. 2; AIAA; Reston, VA; 2002.

[13]AGARD CP 124. April 1973.

[14]Abbott, I. R., and Von Doenhoff, A. E. Theory of Wing Sections. Dover Publications; Mineola, NY; 1949.

CHAPTER 10. AIRCRAFT POWER PLANT AND INTEGRATION

[1]Kundu, A. K. Class Lecture Notes at Queen’s University Belfast. Belfast, UK.

[2]The Jet Engine. Rolls-Royce plc, 5th Edition; 1996.

[3]Cohen H., Rogers, G. F. C., and Saravanamutto, H. I. H. Gas Turbine Theory. Prentice Hall; 2008.

[4]Mattingly, Jack D. Elements of Gas Turbine Propulsion. McGraw-Hill; 1996.

[5]Flack, Ronald D. Fundamentals of Jet Propulsion with Application. Cambridge University Press; 2005.

[6]Hill, P. G., and Peterson, C. R. Mechanics and Thermodynamics of Propulsion. Prentice Hall; 1992.

[7]Oates, Gordon. Aerotherodynamics of Gas Turbines and Rocket Propulsion. AIAA; Reston, VA; 1984.

[8]Swavely, C. E. Propulsion System Overview. Pratt and Whitney short course; 1985.

[9]Farokhi, Saeed, et al. Propulsion System Integration. Short course. University of Kansas; Lawrence, KS; 1991.

[10]Riordan, David. Lecture notes to Queen’s University Belfast. Belfast, UK; 2003.

[11]Whitford, Ray. Design for Combat Aircraft. Jane’s Information Group; Surrey, UK, and Alexandria, VA; 1987.

[12]Jane’s All the World’s Aircraft Manual (later editions). Jane’s Information Group; Surrey, UK, and Alexandria, VA.

[13]McCormick, Barnes W. Aerodynamics, Aeronautics, and Flight Mechanics. Wiley; 1985.

[14]Dommasch, Daniel O., et al. Airplane Aerodynamics. Pitman; New York; 1967.

[15]Perkins, C. D., and Hage, R. E. Aircraft Performance Stability and Control. Wiley; 1949.

[16]Propeller Performance Manual. Hamilton Standard, PD6101A; 1963.

[17]SBAC Standard Method of Performance Estimation. London, UK.

[18]Lan, C. T. E., and Roskam, J. Aeroplane Aerodynamics and Performance; University of Kansas; Lawrence, KS; 1980.

[19]Gunston, Bill. The Development of Jet and Turbine Aero Engines. 4th edition; Hayes North America; Newbury Park, CA; 2006.

[20]Stinton, Darrol. The Design of the Airplane. AIAA; Reston, VA; 2001.

[21]Seddon, J., and Goldsmith, E. Practical Intake Aerodynamic Design. AIAA; Reston, VA; 1965.

[22]Glauert, H. Elements of Aerofoil and Airscrew Theory. 2nd edition; Cambridge University Press; 1983.

[23]Available at www.bh.com/companions/034074152X/appendices; compiled by Lloyd Jenkinson, et al.

CHAPTER 11. AIRCRAFT SIZING, ENGINE MATCHING, AND VARIANT DERIVATIVE

[1]Wallace, Richard E. Parametric and Optimization Techniques for Airplane Design Synthesis. AGARD-LS-56; 1972.

[2]Miele, Angelo. Flight Mechanics, Vol. I: Theory of Flight Paths. AddisonWesley; Reading, MA; 1962.

[3]Perkins, C. D., and Hage, R. E. Airplane Performance, Stability and Control. Wiley; 1949.

[4]Loftin, E.A. NASA TM 1998–207644.

CHAPTER 12. STABILITY CONSIDERATIONS AFFECTING AIRCRAFT CONFIGURATION

[1]Perkins, C. D., and Hage, R. E. Airplane Performance, Stability and Control. Wiley; 1949.

[2]Bernard Etkin. Dynamics of Atmospheric Flight. Dover Publications; 2005.

[3]Nelson, Robert C. Flight Stability and Automatic Control. McGraw-Hill; 1998.

[4]Phillip, Warren F. Mechanics of Flight. Wiley; 2004.

[5]Talay, Theodore A. Introduction to the Aerodynamics of Flight. NASA SP–367; 1975.

[6]Watterson, John. Class Lecture Notes at the Queen’s University Belfast. Belfast, UK.

[7]Munroe, Amy. “Statistics and Trends for Vertical and Horizontal Tails of Commercial Transport and Military Aircraft.” Undergraduate project, with author as a supervisor; May 2006.

[8]Murphy, Steven. “Statistics and Trends for Vertical and Horizontal Tails of Commercial Transport and Military Aircraft.” Undergraduate project, with author as a supervisor; May 2006.

[9]Miele, Angelo. Flight Mechanics, Vol. I: Theory of Flight Paths. AddisonWesley; Reading, MA; 1962.

[10]Collinson, R. P. G. Introduction to Avionics Systems. Kluwer; Boston; 2006.

[11]US DATCOM.

[12]Available at www.centennialofflight.gov/essay/Theories of Flight/Stability II/ TH27G6.htm.

[13]Klug, Heinz G. Messerschmitt Bolkow-Blohm Gmbh. Hamburg, Germany; 1988.

[14]Roskam, J. Aircraft Design. DARcorporation; Lawrence, KS; 2007.

CHAPTER 13. AIRCRAFT PERFORMANCE

[1]Perkins, C. D., and Hage, R. E. Airplane Performance, Stability and Control. Wiley; 1949.

[2]Miele, Angelo. Flight Mechanics, Vol. I: Theory of Flight Paths. AddisonWesley; Reading, MA; 1962.

[3]Roskam, J. Airplane Design, DARcorporation; Lawrence, KS; 2007.

[4]Phillip, Warren F. Mechanics of Flight. Wiley; 2004.

[5]Talay, Theodore A. Introduction to the Aerodynamics of Flight. NASA SP–367; 1975.

[6]Watterson, John. Class Lecture Notes at the Queen’s University Belfast. Belfast, UK.

[7]Bernard, R. H., and Philpot, D. R. Aircraft Flight. Prentice-Hall; 1996.

[8]McCormick, Barnes W. Aerodynamics, Aeronautics and Flight Mechanics. Wiley; 1985.

[9]Hale, F. J. Aircraft Performance, Selection and Design. Wiley; 1984.

CHAPTER 14. COMPUTATIONAL FLUID DYNAMICS

[1]Chapman, D. “Computational Aerodynamics Development and Outlook,” AIAA Journal; Reston, VA; December 1979.

[2]Chapman, D. “A Perspective on Aerospace CFD.” Aerospace America; January 1992.

[3]Roache, Patrick J. Verification and Validation in Computational Science and Engineering. ISBN 0-913478-08-3; 1998.

[4]ARARD AR256. Technical Status Review on Drag Prediction and Analysis from Computational Fluid Dynamics: State of the Art. June 1989.

[5]Melnik, R. E., Siclari, M. J., Marconi, F., Barber, T., and Verhoff, A. “An Overview of a Recent Industry Effort at CFD Code Validation.” AIAA Paper No. 95-2229. 26th AIAA Fluid Dynamic Conference; June 1995.

[6]Thangam, S., and Speziale, C. G. “Turbulent Flow Past a Backward-Facing Step: A Critical Evaluation of Two-Equation Method.” AIAA Journal, Vol. 30, No. 5; May 1992.

[7]Chen, H. C., Yu, N. J., Rubbert, P. E., and Jameson, A. “Flow Simulation of General Nacelle Configurations Using Euler Equations.” AIAA Conference Paper No. 83-0539; 1983.

[8]Uanishi, K., Pearson, N. S, Lahnig, T. R., and Leon, R. M. “CFD-Based 3D Turbofan Nacelle Design System.” AIAA Paper No. A91-16278.

[9]Berman, H., Anderson, J. D., and Drummond, P. A. “Numerical Solution of the Supersonic Flow over a Rearward-Facing Step with Transverse, Nonreacting Hydrogen Injection.” AIAA Paper No. 82-1002; 1982.

[10]Kundu, A. K., Morris, W. H., and Raghunathan, S. “Effect of Manufacturing Tolerances on Aircraft Aerodynamics and Cost.” WMC 97 Conference Paper No. 711–003; 1997.

[11]Cook, T. A. “The Effects of Ridge Excrescences and Trailing Edge Control Gaps on Two-Dimensional Aerofoil Characteristics.” ARC R&M No. 3698; 1971.

[12]Laban, M. “Application of CFD to Drag Analysis and Validation with WindTunnel Data.” Nationaal Lucht-en Ruimtevaartlaboratorium, Von Karman Institute for Fluid Dynamics; Lecture Series; 2003.

[13]Devine, Raymond, et al. “A Comparison of Conventional Pylon Design to a Compression Pylon Design using Computational Fluid Dynamics.” CEIAT; The Queen’s University Belfast. Belfast, UK.

[14]Bell, Mark. “An Investigation into the Complex Aerodynamic Interaction of a Nacelle-Pylon-Wing in Over-Wing Nacelle Configuration.” MEng Thesis. The Queen’s University Belfast. Belfast, UK; May 2006.

[15]Web sites

www.hanleyinnovations.com/multisurface/ msaexperiment01.html www.cfdrc.com/bizareas/aerospace/aeromechanics/

aircraft aerodynamics.html www.esi-group.com/SimulationSoftware/ CFD Fastran/appl aircraft aero.html

CHAPTER 15. MISCELLANEOUS DESIGN CONSIDERATIONS

[1]Smith, Michael J. T. Aircraft Noise. Cambridge University Press; 1983.

[2]Ruijgrok, G. J. J. Elements of Aviation Acoustics. Eburon Academic Publishers; 2003.

[3]ESDU 02020. An Introduction to Aircraft Noise.

[4]Gunston, Bill. The Development of Jet and Turbine Aero Engines. Sparkland Somerset; Patrick Stephens; 2002.

[5]Niu, Michael C. Y. Airframe Structural Design. Commlit Press, Ltd.; Hong Kong; 1999.

[6]Ashby, Michael F. Material Selection in Mechanical Design. Butterworth and Hinemann; Burlington, MA; 1992.

[7]Jukes Malcolm. Aircraft Display Systems. AIAA; Reston, VA; 2004.

[8]Jarrett, D. N. Cockpit Engineering. Ashgate Publishing, Ltd.; 2005.

[9]Moir, Ian, and Seabridge, Allen. Aircraft Systems. Wiley; 2006.

[10]Roskam, Jan. Airplane Design, Vol. 3 and 4. DARcorporation; Lawrence, KS; 2007.

[11]Bingelis, Tony. Engines. EAA; 2000.

[12]Jane’s All the World’s Aircraft Manual, 2001–2002. Jane’s Information Group; Surrey, UK, and Alexandria, VA.

[13]Fielding, John P. Introduction to Aircraft Design. Cambridge University Press; 1999.

[14]McMasters, John H. Boeing Commercial Aircraft, General Engineering Division, Summer Intern Training Program; 1994.

[15]Moir, Ian, and Seabridge, Allen. Civil Avionics Systems. Wiley; Chichester; 2006.

[16]Moir, Ian, and Seabridge, Allen. Military Avionics Systems. Wiley; 2006.

[17]Dhenin, G. (ed.). Aviation Medicine: Health and Clinical Aspects. Tri-Med Books Limited; London; l978.

[18]Society of U.S. Air Force Flight Surgeons. Flight Surgeons Handbook of Life Support Equipment; October 1, 1987.

[19]“Advanced Concept Ejection Seat ACES II.” Report MDC J4576 Revision D; March 1, l988.

[20]Shannon, R. H. “Operational Aspects of Forces on Man During Escape in the U.S. Air Force, l January l968 – 31 December 1970.” In AGARD Linear Acceleration of Impact Type; June l971.

[21]Available at www.fas.org.

CHAPTER 16. AIRCRAFT COST CONSIDERATIONS

[1]Association of European Airlines. “Short–Medium Range Aircraft: AEA Requirements.” 1989.