An aerodynamic assessment of micro-drag generators (MDGs)

16th AIAA Applied Aerodynamics Conference

Volumn , Issue , 1998, Pages

  Bauer, Steven X S ^a  

^a NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; FIGHTER AIRCRAFT; GROUND VEHICLES; LANDING GEAR (AIRCRAFT);

COMMERCIAL TRANSPORT; DEPLOYABLE DEVICES; GENERAL AVIATION; LARGE AMOUNTS; METROPOLITAN AREA; NOISE FOOTPRINTS; SUBSONIC WIND TUNNELS; THRUST REVERSERS;

AERODYNAMIC DRAG;

EID: 84982318039     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1998-2621     Document Type: Conference Paper

References (11)

1. Bauer, S. X. S. and Wood, R. M.: Micro-Drag Generators for Aerobraking and Control. NASA Patent Application LAR 15245-1, 1994.
2. Gentry, G. L.,-Jr.; Quinto, P. F.; Gatlin, G. M.; and Applin, Z. T.: The Langley 14-by 22-Foot Subsonic Tunnel: Description, Flow Characteristics, and Guide for Users. NASA TP-3008. September 1990.
3. McGhee, R. J. and Beasley, W. D.: Low-Speed Aerodynamic Characteristics of a 17-Percent-Thick Airfoil Section Designed for General Aviation Applications. NASA TN D-7428. December 1973.
4. Ayers, T. G.: Supercritical Aerodynamics: Worthwhile Over a Range of Speeds. Astronautics & Aeronautics, vol. 10, no. 8, pages 32-36, August 1972.
5. Hoerner, Dr. S. F.: Fluid-Dynamic Drag, Published by the Author, 1965.
6. Gaudet, L. and Johnson, P.: Measurements of the Drag of Various Two-Dimensional Excrescences Immersed in Turbulent Boundary Layers at Mach Numbers between 0. 2 and 1. 8. RAE TR 70190, 1970.
7. Gaudet, L. and Winter, K. G.: Measurements of the Drag of Some Characteristic Aircraft Excrescences Immersed in Turbulent Boundary Layers. AGARD CP No. 124, Aerodynamic Drag, Paper 4. 1973.
8. Good, M. C. and Joubert, P. N.: The Form Drag of Two-Dimensional Bluff Bodies Immersed in Turbulent Boundary Layers. J. F. M. 31, Pt. 3, pages 547-582. 1968.
9. Jones, R. C. and Williams, D. H.: The Effects of Surface Roughness on Characteristics of Aerofoils NACA 0012 and RAF 34, ARC R&M No. 1708. 1936.
10. Nash, J. F. and Bradshaw, P.: The Magnification of Roughness Drag by Pressure Gradients. J. R. Ae. S. 71, pages 44-49. 1967.
11. Young, A. D. and Paterson, J. H.: Aircraft Excrescence Drag. AGARD-AG-264. 1981.