Analysis for the application of hybrid laminar flow control to a long-range subsonic transport aircraft

Conference · Sun Sep 01 04:00:00 EDT 1991

OSTI ID:7295198

Arcara, Jr, P C; Bartlett, D W; Mccullers, L A ^[1]

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1. NASA, Langley Research Center, Hampton, VA (United States) Vigyan, Inc., Hampton, VA (United States)

The FLOPS aircraft conceptual design/analysis code has been used to evaluate the effects of incorporating hybrid laminar flow control (HLFC) in a 300-passenger, 6500 n. mi. range, twin-engine subsonic transport aircraft. The baseline configuration was sized to account for 50 percent chord laminar flow on the wing upper surface as well as both surfaces of the empennage airfoils. Attention is given to the additional benefits of achieving various degrees of laminar flow on the engine nacelles, and the horsepower extraction and initial weight and cost increments entailed by the HLFC system. The sensitivity of the results obtained to fuel-price and off-design range are also noted. 6 refs.

• Research Organization: National Aeronautics and Space Administration, Hampton, VA (United States). Langley Research Center
• OSTI ID: 7295198
• Report Number(s): CONF-9109281--; SAE-Paper--912113
• Country of Publication: United States
• Language: English

Related Subjects

33 ADVANCED PROPULSION SYSTEMS
330600* -- Advanced Propulsion Systems-- Vehicle Design Factors
AERODYNAMICS
AIRCRAFT
BOUNDARY LAYERS
DESIGN
ENERGY CONSUMPTION
FLUID FLOW
FLUID MECHANICS
FUEL CONSUMPTION
LAMINAR FLOW
LAYERS
MECHANICS