Compressibility and Leading-Edge Bluntness Effects for a 65o Delta Wing

Author:

Luckring James1

Affiliation:

1. NASA Langley Research Center

Publisher

American Institute of Aeronautics and Astronautics

Reference22 articles.

1. 1Polhamus, E. C. "A Concept of the Vortex Lift of Sharp-Edged Delta Wings Based on a Leading-Edge Suction Analogy," NASA TND-3767,1966.

2. 2Hummel, D. "On the Vortex Formation Over aSlenderWingat LargeIncidence,"AGARDCP-247,PaperNo.15,January1979.

3. 3Smith, J. H. B. "Improved Calculations of Leading-Edge SeparationfromSlenderDeltaWings". RAETR-66070,1966.

4. 4Hemsch, M. J., and Luckring, J. M. "Connection Between Leading-Edge Sweep, Vortex Lift, and Vortex Strength for Delta Wings,"AIAA J.Aircraft,Vol.27,No.5,May1990.

5. 5"HighAngleofAttackAerodynamics,"AGARDCP-247,January 1979.

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