Coupled numerical simulation of the external and engine inlet flows for the F-18 at large incidence
Author:
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference23 articles.
1. Erickson GE, Hall RM, Banks DW, Del Frate JH, Schreiner JA, Hanley RJ, Pulley CT. Experimental investigation of the F/A-18 vortex flows at subsonic through transonic speeds. AIAA Paper 89-2222, July–August 1989.
2. Meyn LA, Lanser WR. Full scale high-angle-of-attack tests of an F/A-18. AIAA Paper 92-2676, June 1992.
3. Rizk YM, Guruswamy GP, Gee K. Numerical investigation of the tail buffet on the F-18 aircraft. AIAA paper 92-2673, June 1992.
4. Fisher DF, Del Frate JH, Richwine DM. In-flight flow visualization characteristics of the NASA F-18 high alpha research vehicle at high angles of attack. NASA TM-4193, May 1990.
5. Del Frate JH, Fisher DF, Zuniga FA. In-flight flow visualization with pressure measurements at low speeds on the NASA F-18 high alpha research vehicle. NASA TM-101726, October 1990.
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