NASA NTRS · 19770000423
Compressible laminar boundary-layer flow
Abstract
Program computes compressible laminar boundary-layer flow over yawed infinite wing including distributed suction. Computations are useful in efforts to implement boundary-layer suction on wing to maintain laminar flow in order to reduce net drag. Program contains number of approximations to simplify analysis; yet results are accurate enough to be useful, particularly in preliminary design phase.
Keep this discovery
Explore connections, maps & timelines
Carter, J. E.. 1978-03-01. Compressible laminar boundary-layer flow. https://ntrs.nasa.gov/citations/19770000423
Cite the original work for its findings. Save a collection to share your selection of sources.