Venkit Iyer

发表

Numerical solutions of the compressible 3-D boundary-layer equations for aerospace configurations with emphasis on LFC

Julius E. Harris, Venkit Iyer, Samir Radwan, 1987 .

Implementation of the WICS Wall Interference Correction System at the National Transonic Facility

Venkit Iyer, Norbert Ulbrich, Joel L. Everhart, 2000 .

Computer program BL2D for solving two-dimensional and axisymmetric boundary layers

Venkit Iyer, 1995 .

Improvements to Wall Corrections at the NASA Langley 14 x 22-Ft Subsonic Tunnel

Venkit Iyer, Eric L. Walker, David D. Kuhl, 2003 .

Application of Pressure-Based Wall Correction Methods to Two NASA Langley Wind Tunnels

Venkit Iyer, J L Everhart, V. Iyer, 2001 .

A Wall Correction Program Based on Classical Methods for the National Transonic Facility (Solid Wall or Slotted Wall) and the 14x22-Ft Subsonic Tunnel at NASA LaRC

Venkit Iyer, Michael J. Hemsch, 2004 .

Wall Interference Study of the NTF Slotted Tunnel Using Bodies of Revolution Wall Signature Data

Venkit Iyer, Eric L. Walker, David D. Kuhl, 2004 .

Computational study of transition front on a swept wing leading-edge model

Venkit Iyer, Robert E. Spall, J. R. Dagenhart, 1992 .

Parameter Sensitivity Study of the Wall Interference Correction System (WICS)

Venkit Iyer, Joel L. Everhart, Eric L. Walker, 2001 .

Application of Linear Stability Theory in Laminar Flow Design

Venkit Iyer, Robert E. Spall, 1991 .

Computation of three-dimensional compressible boundary layers to fourth-order accuracy on wings and fuselages

Venkit Iyer, V. Iyer, 1990 .

Transition prediction and control in subsonic flow over a hump

Venkit Iyer, Jamal A. Masad, V. Iyer, 1993 .

Three-Dimensional Boundary-Layer program (BL3D) for swept subsonic or supersonic wings with application to laminar flow control

Venkit Iyer, 1993 .