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General:

Aerodynamics:

  • Abbot, Ira H. and Von Doenhoff, Albert E. (1959) Theory of Wing Sections. NY: Dover Publications, Inc.
  • Fears, Scott P., Holly M Ross and Thomas M. Moul. (1995) Low-Speed Wind-Tunnel Investigation of the Stability and Control Characteristics of a Series of Flying Wings With Sweep Angles of 50°. NASA Technical Memorandum 4640. Hampton, VA: NASA Langley Research Center.
  • Fulghum, David A. (1997a) U.S. Industry Searches for Design Formulas, Aviation Week & Space Technology, June 2, p. 49-50.
  • McCormick, Barnes W. (1995) Aerodynamics, Aeronautics and Flight Mechanics. NY: John Wiley & Sons, Inc.
  • Moul, Thomas M., Scott P. Fears, and Holly M Ross. (1995) Low-Speed Wind-Tunnel Investigation of the Stability and Control Characteristics of a Series of Flying Wings With Sweep Angles of 60°. NASA Technical Memorandum 4640. Hampton VA: NASA Langley Research Center.
  • Raymer, Daniel P. (1992) Aircraft Design: A Conceptual Approach. Washington, DC: American Institute of Aeronautics and Astronautics.
  • Schlichting, Hermann and Erich Truckenbrodt. (1979) Aerodynamics of the Airplane. NY: McGraw-Hill, Inc.

Auxiliary Systems:

  • Flir Systems, Inc. (1998) Airborne Products.
  • Johnson, Chris, ed. (1997) Jane’s Avionics, 16th ed. Surrey, UK: Jane’s Information Group.

Costs:

  • Federal Reserve Board. (1998) FRED - Consumer Price Index Updates.
  • Raymer, Daniel P. (1989) Aircraft Design: A Conceptual Approach. Washington, DC: American Institute of Aeronautics and Astronautics.

Landing Gear:

  • Conway, Hugh Graham. (1958) Landing Gear Design. London: Chapman & Hall.
  • Michelin. (1998) Aviation Tires.
  • Raymer, Daniel P. (1992) Aircraft Design: A Conceptual Approach. Washington, DC: American Institute of Aeronautics and Astronautics.
  • Roskam, Jan. (1989a) Airplane Design Part IV: Layout Design of Landing Gear and Systems. Ottawa, KS: Roskam Aviation and Engineering Corp.

Performance:

  • Anderson, John D., Jr. (1989) Introduction to Flight. NY: McGraw-Hill, Inc.
  • McCormick, Barnes W. (1995) Aerodynamics, Aeronautics and Flight Mechanics. NY: John Wiley & Sons, Inc.
  • Raymer, Daniel P. (1992) Aircraft Design: A Conceptual Approach. Washington, DC: American Institute of Aeronautics and Astronautics.

Propulsion:

  • Oates, C. Gordan. (1988) Aerothermodynamics of Gas Turbine and Rocket Propulsion. Washington, DC: American Institute of Aeronautics and Astronautics.
  • Pratt and Whitney. (1998) Nozzles.
  • Raymer, Daniel P. (1992) Aircraft Design: A Conceptual Approach. Washington, DC: American Institute of Aeronautics and Astronautics.

Stability & Control:

  • Etkin, Bernard and Lloyd Duff Reid. (1996) Dynamics of Flight: Stability and Control. NY: John Wiley & Sons, Inc.
  • Fears, Scott P., Holly M Ross and Thomas M. Moul. (1995) Low-Speed Wind-Tunnel Investigation of the Stability and Control Characteristics of a Series of Flying Wings With Sweep Angles of 50°. NASA Technical Memorandum 4640. Hampton, VA: NASA Langley Research Center.

Stealth:

  • Aronstein, David C. and Albert C. Piccirillo. (1997) Have Blue and the F-117A: Evolution of the "Stealth Fighter". Washington DC: American Institute of Aeronautics and Astronautics.
  • Fulghum, David A. (1997a) U.S. Industry Searches for Design Formulas, Aviation Week & Space Technology, June 2, p. 49-50.

Structures:

  • _____. (1998) Advanced Composite Supplies. Fortville, IN: Applied Vehicle Technology.
  • Brown, William F., Jr., ed. (1997) Aerospace Structures Materials Handbook, Vol. 3. West Lafayette, IN: CINDAS/USAF CRDA Handbook Operation.
  • Bruhn, Elmer F. (1965) Analysis and Design of Flight Vehicle Structures. Cincinnati, OH: Tri-State Offset Co.
  • Donaldson, Bruce K. (1993) Atlas of Stress-Corrosion and Corrosion Fatigue Curves. Materials Park, OH: ASM International.
  • Niu, Michael Chun-Yung. (1991) Airframe Structural Design. Hong Kong: Conmilt Press.
  • Peery, D. J. (1950) Aircraft Structures. NY: McGraw-Hill, Inc.
  • Raymer, Daniel P. (1992) Aircraft Design: A Conceptual Approach. Washington, DC: American Institute of Aeronautics and Astronautics.
  • Roskam, Jan. (1989b) Airplane Design Part V: Component Weight Estimation. Ottawa, KS: Roskam Aviation and Engineering Corp.

Weight & Balance:

  • Raymer, Daniel P. (1989) Aircraft Design: A Conceptual Approach. Washington, DC: American Institute of Aeronautics and Astronautics.




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