Theoretical prediction of over-wing-blowing aerodynamics

Author:

LAN C.1,FILLMAN G.1,CAMPBELL J.2

Affiliation:

1. Kansas, University, Laurence, Kan.

2. NASA, Langley Research Center, Subsonic-Transonic Aerodynamics Div., Hampton, Va.

Publisher

American Institute of Aeronautics and Astronautics

Reference30 articles.

1. action for Engine Configurations nounted above the Wing," Paper No. 26 in AGARD CP-150. AirframelPropuls 1on Interference. Septenbec 1914. Putnam. L.E. "Exploratory 'Investigation at Xach 2

2. Numbers from 0.40 to 0.95 of the'Effects of Jets Blown over a Wing," NASA November 1973.

3. "Effects of Upper-Surface alowing and %:*st Vectorfng on Low-Speed Aerodvnamic Charaetrristics of a Large-Scale Supersonic Transpart Yodel.'* XASA PI X-72792,Sovrnber 1975. 'Struck, H. and Klcvenhusen. K.D. "The Prediction

4. Cross Flow," NASA TR R-613. December 1973. v

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