Flight tests with a natural laminar flow glove on a transport aircraft

Flight Simulation Technologies Conference and Exhibit, 1990

Volumn , Issue , 1990, Pages 385-392

  Horstmann, K H ^a   Redeker, G ^a   Quast, A ^a   Dressler U ^b   Bieler, H ^b  

^a GERMAN AEROSPACE CENTER DLR   (Germany)

^b AIRBUS OPERATIONS GMBH   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYER FLOW; BOUNDARY LAYERS; INFRARED IMAGING; LAMINAR FLOW; REYNOLDS NUMBER; SOFTWARE TESTING; STABILITY; TRANSPORT AIRCRAFT;

ATTACHMENT LINES; BOUNDARY LAYER INSTABILITY; CROSS-FLOW INSTABILITIES; NATURAL LAMINAR FLOWS; STABILITY ANALYSIS; STABILITY CALCULATION; TRANSITION LOCATIONS; TRANSITION PREDICTION;

FLIGHT SIMULATORS;

EID: 85002406438     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1990-3044     Document Type: Conference Paper

References (11)

1. Körner, H.: Natural Laminar Flow Research for Subsonic Transport Aircraft in the FRG. Lecture at 16th Congress of ICAS, August 28-September 2, 1988, Jerusalem, Israel.
2. Redeker, G.; Horstmann, K.H.; Köster, H.; Thiede, P.; Szodruch, J.: Design of a natural laminar flow glove for a transport aircraft. AIAA-paper No. 90-3043, 1990.
3. Cumpsty, N.A.; Head, M. R.: The calculation of three-dimensional turbulent boundary layers. Part II: Attachment line flow on an infinite swept wing. The Aeronautical Quart., Vol. 18, (1967), pp. 150-164.
4. Pfenninger, W.: Some results from the X-21 program. Part I: Flow phenomena at the leading edge of swept wings. In: “Recent developments in boundary layer research”. Part IV:, AGARDo-graph 97, May 1965.
5. Poll, D.I.A.: Transition in the infinite swept attachment line boundary layer. The Aeronautical Quart., Vol. 30, 1979, pp. 607-629.
6. Horstmann, K.H.; Quast, A.; Redeker, G.: Flight and Wind-Tunnel Investigations on Boundary-Layer Transition. Journ. Aircraft, Vol. 27, 1990, pp. 146-150.
7. Quast, A.: Detection of transition by infrared image technique. ICIASF Proceedings, June 22-25, 1987, Williamsburg.
8. Henke, R.; Münch, F.X.; Quast, A.: Natural Laminar Flow: A Wind Tunnel Test Campaign and Comparison with Flight Test Data. AIAA-paper No. 90-3045, 1990.
9. Coustols, E.: Stabilité et transition en écoulement tridimensionel: Cas des ailes en flèche. Thèse présentée à 1’école national supérieure de l’aéronautique et de l’espace, Toulouse.
10. Skrokowski, A.J.; Orszag, S.A.: SALLY level II user’s guide. COSMIC Program No. LAR-12556, 1979.
11. Kreplin, H.-P.; Höhler, G.: Oberflä-chenheißfilmmessungen am ATTAS-Laminarhandschuh im Freiflug und Windkanal. DGLR-Vortr. Nr. 89 188, DGLR-1989 II.