Configuration development of a supersonic cruise strike-fighter

Author:

MEYER R.1,FIELDS W.2

Affiliation:

1. Grumman Aerospace Corp., Bethpage, N.Y.

2. USAF, Flight Dynamics Laboratory, Wright-Patterson AFB, Ohio

Publisher

American Institute of Aeronautics and Astronautics

Reference40 articles.

1. Carlson, H.W., LongitudinalAerodynamicCharacterisricsatMachNumber 2.02of aSeriesof Wing-SodyConfigurationsEmployinga CamberedandTwistedArrow Wing. NASATMX.836, May 1963.

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1. Strake camber and thickness design procedure for low alpha supersonic flow;Journal of Aircraft;1990-06

2. ATTENTION JOURNAL AUTHORS;Journal of Aircraft;1990-06

3. Piloted simulator evaluation of a relaxed static stability fighter at high angle-of-attack;9th Atmospheric Flight Mechanics Conference;1982-08-09

4. Propulsion integration of a supersonic cruise strike-fighter;17th Aerospace Sciences Meeting;1979-01-15

5. Design study results of a supersonic cruise fighter wing;17th Aerospace Sciences Meeting;1979-01-15

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