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.

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

Kenneth J. Baumeister and Kevin L. Kreider.

Development of a low-Reynolds number, nonlinear [kappa-epsilon] model for the reduced Navier-Stokes equations: a final technical report for NASA-LeRC grant NAG-1781

David A. Boger, T.R. Govindan, and Henry McDonald.

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.

Effects of initial conditions on a single jet in crossflow

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

Improved NASA-ANOPP noise prediction computer code for advanced subsonic propulsion systems

K. B. Kontos

Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6

Scott D. Holland.

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