A design methodology for semi-span model mounting geometries

36th AIAA Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 1998, Pages

  Milholen, William E ^a  

^a NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING; NAVIER STOKES EQUATIONS;

COMMERCIAL TRANSPORT; COMPUTATIONAL RESULTS; COMPUTATIONAL STUDIES; DESIGN METHODOLOGY; PARAMETRIC FAMILY; SPAN CONFIGURATION; STREAMLINE PATTERN; THREE-DIMENSIONAL NAVIER-STOKES;

BOUNDARY LAYERS;

EID: 84983203532     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (8)

1. th International Council of the Aeronautical Sciences, Paper 90-2.6.2, Sept. 1990, pp. 1028-1042.
2. Ulbrich, N. and Steinle, F.W., Jr., "Semispan Model Wall Interference Prediction Based on the Wall Signature Method," AIAA Paper 95-0793, Jan. 1995.
3. Milholen, W.E., II, Chokani, N., and McGhee, R.J., "Development of Semispan Model Test Techniques," Journal of Aircraft, Vol. 33, No. 6, 1996, pp.1115-1122.
4. Vatsa, V.N., Sanetrik, M.D., and Parlette, E.B., "Development of a Flexible and Efficient Multigrid-Based Multiblock Flow Solver," AIAA Paper 93-0677, Jan. 1993.
5. Milholen, W.E., II, Chokani, N., and Al-Saadi, J.A., "Performance of Three-Dimensional Compressible Navier-Stokes Codes at Low Mach Numbers," AIAA Journal, Vol. 34, No. 7, 1996, pp. 1356-1362.
6. Steinbrenner, J.P. and Chawner, J.R., "Incorporation of a Hierarchical Grid Component Structure into GRIDGEN," AIAA Paper 93-0429, Jan. 1993.
7. Shabaka, I.M.M.A. and Bradshaw, P., "Turbulent Flow Measurements in an Idealized Wing/Body Junction," AIAA Journal, Vol. 19, No.2, pp. 131-132.
8. Campbell, R.L, "Efficient Constrained Design Using Navier-Stokes Codes," AIAA Paper 95-1808, 1995.