Energy-Maneuverability theory

Energy Maneuverability theory is a model of aircraft performance. It was promulgated by Col. John Boyd, and is useful in describing an aircraft's ability to acquire and preserve aircraft specific energy.

It relates the thrust, weight, drag, wing area, and other flight characteristics of an aircraft into a quantitative model. This allows combat capabilities of various aircraft or prospective design trade-offs to be predicted and compared.

::$P\_s\; =\; [frac\{T\; -\; D\}\; W]\; V$

Specific power equals thrust minus drag, divided by the aircraft's weight, times the current velocity. Power is a force times a velocity; any parameter termed "specific" is normalized to either the mass or weight, hence the "s" subscript.

Boyd, a skilled US jet fighter pilot in the Korean war, went on to pioneer the use of computer modeling to predict aircraft performance. His work at Eglin air force base in the early 1960's, charting the performance envelopes of US and Soviet aircraft, produced conclusions that were unwelcome but ultimately undeniable. Boyd's theories, coupled with his persistence, brought about crucial design improvements in the F-15 and F-16 jet fighters.

References

*Hammond, Grant T. "The Mind of War: John Boyd and American Security". Washington, D.C.: Smithsonian Institution Press, 2001. ISBN 1-56098-941-6 and ISBN 1-58834-178-X. An explanation of Boyd's ideas.

* Coram, Robert. "Boyd: The Fighter Pilot Who Changed the Art of War". New York: Back Bay Books, 2002. ISBN 0-316-88146-5 and ISBN 0-316-79688-3. A biography.

* Wendl, M.J., Grose, G.G., Porter, J.L., and Pruitt, V.R. (1974) [http://www.sae.org/technical/papers/740480 "Flight/Propulsion Control Integration Aspects of Energy Management"] , Society of Automotive Engineers paper number 740480.