Computational design and analysis of a transonic natural laminar flow wing for a wind tunnel model

MN Lynde, RL Campbell - 35th AIAA Applied Aerodynamics …, 2017 - arc.aiaa.org
S environmental concerns grow and gas prices rise, the need for more efficient transonic
transports becomes increasingly prevalent. Industry and research partners work to keep up …

Natural laminar flow design for wings with moderate sweep

RL Campbell, MN Lynde - 34th AIAA Applied Aerodynamics …, 2016 - arc.aiaa.org
I. Introduction s the cost of fuel continues to increase over time and concern for the
environment drives acceptable levels of emissions lower, the goal of reducing drag and the …

Numerical study of the turbulent transonic interaction and transition location effect involving optimisation around a supercritical aerofoil

D Szubert, I Asproulias, F Grossi, R Duvigneau… - European Journal of …, 2016 - Elsevier
The present article analyses the turbulent flow around a supercritical aerofoil at high
Reynolds number and in the transonic regime, involving shock-wave/boundary-layer …

Transonic Cruise Slotted Wing Design for Commercial Transport Aircraft using CDISC

BR Hiller, RL Campbell, MN Banchy - AIAA SCITECH 2024 Forum, 2024 - arc.aiaa.org
A knowledge-based aerodynamic design method, CDISC, has been extended to enable the
computational design of transonic cruise slotted wings for commercial transport aircraft. The …

An inverse design method with aerodynamic design optimization for wing glove with hybrid laminar flow control

Y Yang, J Bai, L Li, T Yang, H Wang, S Ma… - Aerospace Science and …, 2019 - Elsevier
The design of the hybrid laminar flow control (HLFC) system involves the comprehensive
design of the suction control and the profile, and it has become an urgent problem for a three …

Laminar flow control flight experiment design and execution

AA Tucker, WS Saric, HL Reed - 52nd aerospace sciences meeting, 2014 - arc.aiaa.org
Previous flight research programs have sampled laminar flow control at a single control
point, usually a cruise condition. In the case of the presently discussed swept-wing-glove …

Design of an infinite-swept-wing glove for in-flight discrete-roughness-element experiment

MW Tufts, HL Reed, WS Saric - Journal of Aircraft, 2014 - arc.aiaa.org
The Subsonic Aircraft Roughness Glove Experiment is an in-flight experiment designed to
meet the NASA Environmentally Responsible Aviation project requirements. The goal of the …

Active control of laminar separation: simulations, wind tunnel, and free-flight experiments

A Gross, HF Fasel - Aerospace, 2018 - mdpi.com
When a laminar boundary layer is subjected to an adverse pressure gradient, laminar
separation bubbles can occur. At low Reynolds numbers, the bubble size can be substantial …

Computational evaluation and linear stability of a transonic laminar-flow wing glove

MW Roberts, HL Reed, WS Saric - Journal of Aircraft, 2015 - arc.aiaa.org
The Flight Research Laboratory at Texas A&M University has proposed conducting both
natural laminar flow and passive laminar flow control flight-test experiments through NASA's …

Design of Experiments with an Application to Laminar Flow Control Flight Research

AA Tucker, HL Reed, WS Saric, DT Ward - AIAA Atmospheric Flight …, 2016 - arc.aiaa.org
Previous flight research programs have sampled laminar flow control at a single control
point, usually a cruise condition. Tucker, et al.[1],[2] developed a laminar flow control flight …