Jet aeroacoustics

Ganesh Raman

New Results in Numerical and Experimental Fluid Mechanics V

Heinz Hönlinger

Aircraft loading and structural layout

Denis Howe

Lobed mixer design for noise suppression

Vinod Govind Mengle

Turbulent Navier-Stokes flow analysis of an advanced semispan diamond-wing model in tunnel and free air at high-lift conditions

Farhad Ghaffari

Acoustic and laser doppler anemometer results for confluent, 22-lobed, and unique-lobed mixer exhaust systems for subsonic jet noise reduction

Aerodynamic measurements on a large splitter plate for the Langley Transonic Dynamics Tunnel

D. M. Schuster

Inviscid flow computations of the orbital sciences X-34 over a Mach number range of 1.25 to 6.0

Ramadas K. Prabhu

Computational aeroacoustics by the space-time CE/SE method

Loh, Ching, Y.

Use of a scale model in the design of modifications to the NASA Glenn Icing Research Tunnel

Victor A. Canacci

Aerodynamic calibration of the NASA Lewis icing research tunnel (1997 tests)

Jose C. Gonsalez

Wind-tunnel investigations of blunt-body drug reduction using forebody surface roughness

Stephen A. Whitmore

Flight, wind-tunnel, and computational fluid dynamics comparison for cranked arrow wing (F-16XL-1) at subsonic and transonic speeds

Aerodynamic shape optimization of two-dimensional airfoils under uncertain conditions

Luc Huyse

Summary report of the orbital X-34 wing static aeroelastic study

Ramadas K. Prabhu

Development and demonstration of active noise control concepts

Aerodynamic lift and moment calculations using a closed-form solution of the Possio equation

Jensen Lin

Ice accretions and icing effects for modern airfoils

Harold E. Addy

Description of panel method code ANTARES

Norbert Ulbrich

In-flight aerodynamic measurements of an iced horizontal tailplane

Thomas P. Ratvasky

Large-scale parallel unstructured mesh computations for 3D high-lift analysis

Dimitri Mavriplis

In-flight aerodynamic measurements of an iced horizontal tailplane

Thomas P. Ratvasky

First NASA/Industry High-Speed Research Configuration Aerodynamics Workshop

NASA/Industry High-Speed Research Configuration Aerodynamics Workshop (1st 1996 Hampton, Va.)

Reassessment of heavy-duty truck aerodynamic design features and priorities

Edwin J. Saltzman

Development of a linearized unsteady Euler analysis with application to wake/blade-row interactions

Joseph M. Verdon

Factors affecting inlet-engine compatibility during aircraft departures at high angle of attack for an F/A-18A aircraft

First NASA/Industry High-Speed Research Configuration Aerodynamics Workshop

NASA/Industry High-Speed Research Configuration Aerodynamics Workshop (1st 1996 Hampton, Va.)

Reassessment of heavy-duty truck aerodynamic design features and priorities

Edwin J. Saltzman

Two-dimensional fourier transform applied to helicopter flyover noise

Odilyn L. Santa Maria

Design of supersonic transport flap systems for thrust recovery at subsonic speeds

Michael J. Mann

Active control of fan noise by vane actuators

Alan R. D. Curtis

Follow-on low noise fan aerodynamic study

Nathan J. Heidegger

Computational assessment of aft-body closure for the HSR reference H configuration

W. Kelly Londenberg

Subsonic investigation of leading-edge flaps designed for vortex- and attached-flow on a high-speed civil transport configuration

Implementation of a trailing-edge flap analysis model in the NASA Langley CAMRAD.MOD1/HIRES program

Bruce Charles

Two-dimensional fourier transform applied to helicopter flyover noise

Odilyn L. Santa Maria

Navier-Stokes analysis of the flowfield characteristics of an ice contaminated aircraft wing

1999 NASA High-Speed Research Program Aerodynamic Performance Workshop

NASA High-Speed Research Program Aerodynamic Performance Workshop (1999 Anaheim, Calif.)

1999 NASA High-Speed Research Program Aerodynamic Performance Workshop

NASA High-Speed Research Program Aerodynamic Performance Workshop (1999 Anaheim, Calif.)

Development of a linearized unsteady Euler analysis with application to wake/blade-row interactions

Joseph M. Verdon

Large-scale parallel unstructured mesh computations for 3D high-lift analysis

Dimitri Mavriplis

Base drag reduction experiment on the X-33 Linear Aerospike SR-71 Experiment (LASRE) flight program

Stephen A. Whitmore

Analysis of wind tunnel oscillatory data of the X-31A aircraft

Mark S. Smith

Simultaneous optical measurements of axial and tangential steady-state blade deflections

Anatole P. Kurkov

Navier-Stokes simulation of several high-lift reference H configurations

Wendy B. Lessard

Reassessment of heavy-duty truck aerodynamic design features and priorities

Edwin J. Saltzman

Active control of fan noise by vane actuators

Alan R. D. Curtis

Aerothermodynamic calculations on X-34 at Mach 6 wind tunnel conditions

William A. Wood

Large-scale parallel unstructured mesh computations for 3D high-lift analysis

Dimitri Mavriplis

Evaluation of the Tone Fan Noise Design/Prediction System (TFaNS) at the NASA Glenn Research Center

L. Danielle Koch

Experimental and numerical study of icing effects on the performance and controllability of a twin engine aircraft

TFaNS T̲one F̲a̲n N̲oise Design/Prediction S̲ystem

David A. Topol

Boeing 18-inch fan rig broadband noise test

Preliminary in-flight loads analysis of in-line launch vehicles using the VLOADS 1.4 program

J. B. Graham

Acoustics of fluid-structure interactions

M. S. Howe

Two-dimensional high-lift aerodynamic optimization using neural networks

Roxana M. Greenman

Mechanical design of high lift systems for high aspect ratio swept wings

Peter K. C. Rudolph

Simulation-based analysis of reentry dynamics for the SHARP atmospheric entry vehicle

Clemens Emmanuel Tillier

Design selection and analysis of a swept and leaned stator concept

Edmane Envia

Broadband fan noise generated by small scale turbulence

Stewart A. L. Glegg

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