A Thin Airfoil with a Minimum Average Coefficient of Heat Transfer for a Given Lift.

E. V. Bulygina, Joy B. Gazley

ResearchPublished 1962

An analysis of the aerodynamic heating of a wing profile at supersonic speeds and the determination of the wing profile for a minimum average heat transfer to the wing. An analysis of the aerodynamic heating of a wing profile at supersonic speeds and the determination of the wing profile for a minimum average heat transfer to the wing. 18 pp.

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  • Copyright: RAND Corporation
  • Availability: Available
  • Year: 1962
  • Print Format: Paperback
  • Paperback Pages: 18
  • Paperback Price: $20.00
  • Document Number: RM-3410-PR

Citation

RAND Style Manual
Bulygina, E. V. and Joy B. Gazley, A Thin Airfoil with a Minimum Average Coefficient of Heat Transfer for a Given Lift. RAND Corporation, RM-3410-PR, 1962. As of September 5, 2024: https://www.rand.org/pubs/research_memoranda/RM3410.html
Chicago Manual of Style
Bulygina, E. V. and Joy B. Gazley, A Thin Airfoil with a Minimum Average Coefficient of Heat Transfer for a Given Lift. Santa Monica, CA: RAND Corporation, 1962. https://www.rand.org/pubs/research_memoranda/RM3410.html. Also available in print form.
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