The production of aerodynamic forces by heat addition on external surfaces of aircraft.

W. W. Willmarth

ResearchPublished 1957

A development of an equivalence between a fluid-mass source, a heat source, and streamwise body forces within the framework of linearized flow theory. Examples for a two-dimensional flat plate, a delta wing, an axially symmetric slender body, and a wedge-shaped afterbody are computed at subsonic and supersonic speeds.

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  • Copyright: RAND Corporation
  • Availability: Available
  • Year: 1957
  • Print Format: Paperback
  • Paperback Pages: 44
  • Paperback Price: $23.00
  • Document Number: RM-2078

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RAND Style Manual
Willmarth, W. W., The production of aerodynamic forces by heat addition on external surfaces of aircraft. RAND Corporation, RM-2078, 1957. As of October 13, 2024: https://www.rand.org/pubs/research_memoranda/RM2078.html
Chicago Manual of Style
Willmarth, W. W., The production of aerodynamic forces by heat addition on external surfaces of aircraft. Santa Monica, CA: RAND Corporation, 1957. https://www.rand.org/pubs/research_memoranda/RM2078.html. Also available in print form.
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