Leading edges

Computation of separated and unsteady flows with one- and two-equation turbulence models: 32nd Aerospace Sciences meeting & exhibit, January 10-13, 1994/Reno, NV

J.A. Ekaterinaris and F.R. Menter.

Receptivity of flat-plate boundary layer in a non-uniform free stream (vorticity normal to the plate): under cooperative agreement NCC1-241

M.N. Kogan and M.V. Ustinov.

High-lift systems on commercial subsonic airliners

Peter K.C. Rudolph.

3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet

M. Mizukami and J.D. Saunders.

Finite element elastic-plastic-creep and cyclic life analysis of a cowl lip

Vinod K. Arya and Matthew E. Melis and Gary R. Halford.

The structure of separated flow regions occurring near the leading edge of airfoils, including transition: semi-annual status report, November 1984 - April 1985

principal investigator, Thomas J. Mueller.

Airfoil modification effects on subsonic and transonic pressure distributions and performance for the EA-6B airplane

Dennis O. Allision and William G. Sewall.

Effect of actuated forebody strakes on the forebody aerodynamics of the NASA F-18 HARV

David F. Fisher, Daniel G. Murri, and Wendy R. Lanser.

The response of the unsteady laminar boundary layer to leading edge acoustic diffraction

Steven John Hulshoff.

Task 4 supporting technology

P.A. Hogenson, principal investigator.