Engine inlets

NASA Lewis Propulsion Systems Laboratory customer guide manual

Ronald H. Soeder.

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

M. Mizukami and J.D. Saunders.

Final technical report on grant NAG3-1567 entitled Inlet distortion in engines on VSTOL aircraft

submitted to NASA Lewis Research Center ; principal investigator Choon S. Tan, co-investigator Edward M. Greitzer.

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

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

Effects of initial conditions on a single jet in crossflow

D.S. Liscinsky and B. True, J.D. Holdeman.

Time-dependent parabolic finite difference formulation for harmonic sound propagation in a two-dimensional duct with flow

Kenneth J. Baumeister and Kevin L. Kreider.

Mach 10 experimental database of a three-dimensional scramjet inlet flow field

Scott D. Holland.

High Reynolds number investigation of a flush-mounted, S-duct inlet with large amounts of boundary layer ingestion

Bobby L. Berrier, Melissa B. Carter, and Brian G. Allan

Fan noise prediction system development: source/radiation field coupling and workstation conversion for the acoustic radiation code

H.D. Meyer.

Finite difference time marching in the frequency domain: a parabolic formulation for aircraft acoustic nacelle design

Kenneth J. Baumeister and Kevin L. Kreider.