Walter C. Engelund

发表

Rocket-powered single-stage vehicle configuration selection and design

Douglas O. Stanley, Walter C. Engelund, Roger A. Lepsch, 1993 .

Verification of a CFD Procedure for Aerodynamic Database Development Using the Hyper-X Stack Configuration

Paresh Parikh, Walter C. Engelund, Robert D. Bittner, 2004 .

Aerodynamic predictions and experimental results for an Advanced Manned Launch System orbiter configuration

Walter C. Engelund, George M. Ware, 1993 .

Experimental Aerodynamic Characteristics of the Pegasus Air-Launched Booster and Comparisons with Predicted and Flight Results

Walter C. Engelund, Michael R. Mendenhall, M. N. Rhode, 1995 .

Propulsion requirements for reusable single-stage-to-orbit rocket vehicles

Douglas O. Stanley, Walter C. Engelund, Roger A. Lepsch, 1994 .

Integrated Aeropropulsive Computational Fluid Dynamics Methodology for the Hyper-X Flight Experiment

Walter C. Engelund, Robert D. Bittner, Charles E. Cockrell, 2001 .

Hyper-X Research Vehicle Experimental Aerodynamics Test Program Overview

Walter C. Engelund, William C. Woods, Scott D. Holland, 2001 .

Design for Quality Using Response Surface Methods: An Alternative to Taguchi's Parameter Design Approach

Douglas O. Stanley, Walter C. Engelund, Roger A. Lepsch, 1994 .

Aerodynamic database development for the Hyper-X airframe integrated scramjet propulsion experiments

Walter C. Engelund, Robert D. Bittner, Charles E. Cockrell, 2000 .

Evaluation of a CFD Method for Aerodynamic Database Development using the Hyper -X Stack Configuration

Paresh Parikh, Walter C. Engelund, Robert D. Bittner, 2004 .

Propulsion system requirements for reusable single-stage-to-orbit rocket vehicles

Douglas O. Stanley, Walter C. Engelund, Roger A. Lepsch, 1992 .

Aerodynamics for a Winged, Circular-Body, Single-Stage-to-Orbit Spacecraft Configuration

Walter C. Engelund, W. P. Phillips, W. Pelham Phillips, 1997 .

Enhancements to the high speed convective heating and viscous drag prediction techniques of the Aerodynamic Preliminary Analysis System (APAS)

Walter C. Engelund, Christopher I. Cruz, 1991 .

Aerodynamic configuration design using response surface methodology analysis

Douglas O. Stanley, Walter C. Engelund, Roger A. Lepsch, 1993 .

Design and Analysis of the Drop Test Vehicle for the Mars Exploration Rover Parachute Structural Tests

Walter C. Engelund, Juan R. Cruz, David W. Way, 2003 .

Aerothermoelastic analysis of a NASP demonstrator model

Walter C. Engelund, Anthony S. Pototzky, Thomas A. Zeiler, 1993 .

2-D and 3-D mixing flow analyses of a scramjet-afterbody configuration

Walter C. Engelund, Oktay Baysal, Mohamed E. Eleshaky, 1989 .

Hyper-X Wind Tunnel Program

Walter C. Engelund, Lawrence D. Huebner, Scott D. Holland, 1998 .

Approximation model building and multidisciplinary design optimization using response surface methods

Douglas O. Stanley, Walter C. Engelund, Roger A. Lepsch, 1996 .

Hyper-X Research Vehicle (HXRV) experimental aerodynamics test program overview

Walter C. Engelund, William C. Woods, Scott D. Holland, 2000 .

Wind tunnel testing, flight scaling and flight validation with Hyper-X

Walter C. Engelund, J. White, Scott D. Holland, 1998 .

Entry, Descent and Landing Systems Analysis Study: Phase 2 Report on Exploration Feed-Forward Systems

Walter C. Engelund, Richard W. Powell, Thomas A. Zang, 2011 .

Stage Separation Analysis of the X-43A Research Vehicle

Walter C. Engelund, John G. Martin, Peter A. Liever, 2004 .

Mars Pathfinder six-degree-of-freedom entry analysis

Walter C. Engelund, Richard W. Powell, Robert D. Braun, 1995 .

Six degree-of-freedom atmospheric entry analysis for the Mars Pathfinder mission

Walter C. Engelund, Richard W. Powell, Robert D. Braun, 1995 .

Mars Ascent Vehicle Flight Analysis

Walter C. Engelund, Robert D. Braun, Prasun N. Desai, 1998 .

An Aerodynamic Preliminary Analysis System (APAS) calibration report - Space Shuttle Orbiter

Walter C. Engelund, Christopher I. Cruz, 1992 .

Hyper-X aerodynamics: The X-43A airframe-integrated scramjet propulsion flight-test experiments

Walter C. Engelund, W. Engelund, 2001 .

Adaptive computations of multispecies mixing between scramjet nozzleflows and hypersonic freestream

Walter C. Engelund, Mohamed E. Eleshaky, M. E. Eleshaky, 1989 .

Mars Entry Atmospheric Data System Modelling and Algorithm Development

Walter C. Engelund, Christopher D. Karlgaard, Paul M. Siemers, 2009 .

Navier-Stokes calculations of scramjet-afterbody flowfields

Walter C. Engelund, Oktay Baysal, K. Tatum, 1988 .