Research in natural laminar flow and laminar-flow control, part 3

Conference · Tue Dec 01 00:00:00 EST 1987

OSTI ID:7071064

Hefner, J N; Sabo, F E

Part 3 of the Symposium proceedings contains papers addressing advanced airfoil development, flight research experiments, and supersonic transition/laminar flow control research. Specific topics include the design and testing of natural laminar flow (NLF) airfoils, NLF wing gloves, and NLF nacelles; laminar boundary-layer stability over fuselage forebodies; the design of low noise supersonic/hypersonic wind tunnels; and boundary layer instability mechanisms on swept leading edges at supersonic speeds.

• Research Organization: National Aeronautics and Space Administration, Hampton, VA (USA). Langley Research Center
• OSTI ID: 7071064
• Report Number(s): N-90-12539; NASA-CP-2487-PT-3; L-16350-PT-3; NAS-1.55:2487-PT-3; CONF-8703331-
• Resource Relation: Conference: Research in natural laminar flow and laminar-flow control conference, Hampton, VA (USA), 16-19 Mar 1987
• Country of Publication: United States
• Language: English

Related Subjects

42 ENGINEERING
LAMINAR FLOW
MEETINGS
BOUNDARY LAYERS
LEADING ABSTRACT
REYNOLDS NUMBER
SUPERSONIC FLOW
ABSTRACTS
DOCUMENT TYPES
FLUID FLOW
LAYERS
420400* - Engineering- Heat Transfer & Fluid Flow