Propfan installation aerodynamics of a supercritical swept wing transport configuration
Author:
Affiliation:
1. NASA, Ames Research Center, Moffett Field, CA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1981-1563
Reference6 articles.
1. 'Welge, H. Robert, Neuhart, Dan H., and Dahlin, John A, "Analysis of Mach Number 0.8 Turboprop Slipstream WingINacelle Interactions," NASA CR-166214 (to be published).
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1. Calculations of propeller/airframe interference effects using the potential/multienergy flow method;AIAA Journal;1990-05
2. Computation of prop-fan engine installation aerodynamics;Journal of Aircraft;1986-04
3. Flow simulations for nacelle-propeller configurations using Euler equations;2nd Applied Aerodynamics Conference;1984-08-17
4. Method for calculating effects of a propfan on aircraft aerodynamicsat subsonic speeds;19th Joint Propulsion Conference;1983-06-27
5. Transonic flow simulation of prop-fan configurations;21st Aerospace Sciences Meeting;1983-01-10
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