Cover Image

Automated boundary conditions for wind tunnel simulations /

Bibliographic Details
Main Author:	Carlson, Jan-Renee (Author)
Format:	Government Document eBook
Language:	English
Published:	Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, March 2018.
Series:	NASA technical memorandum ; 2018-219812.
Subjects:	Boundary conditions. Computational fluid dynamics. Wind tunnels. Simulation. Mach number.
Online Access:	https://purl.fdlp.gov/GPO/gpo90359

Similar Items

Nozzle plume/shock interaction experimental and computational sonic boom analyses from the NASA Ames 9-by 7-foot supersonic wind tunnel /
by: Durston, D. A.
Published: (2018)

Measurements of fluctuating pressures in 8- by 6-foot supersonic wind tunnel for Mach number range of 0.56 to 2.07 /
by: Karabinus, Raymond J., et al.
Published: (1970)

A fan pressure ratio correlation in terms of Mach number and Reynolds number for the Langley 0.3-Meter Transonic Cryogenic Tunnel /
by: Lawing, Pierce L., et al.
Published: (1980)

NASA Glenn 1-by 1-foot supersonic wind tunnel user manual /
by: Seablom, Kirk D.
Published: (1999)

Effectiveness of a wedge probe to measure sonic boom signatures in a supersonic wind tunnel /
by: Wilcox, Floyd J. (Floyd Jay)
Published: (2013)

Results of aeroheating DFI and ET design-data test on a 0.0175-scale model 60-OTS conducted in the Von Karman gas dynamics facility (VKF) 40-inch supersonic and the 50-inch hypersonic wind tunnels A & C (IH-97A/B/C) /
by: Marroquin, J.
Published: (1985)

Uncertainty analysis of the NASA Glenn 8X6 supersonic wind tunnel /
by: Stephens, Julia Elizabeth
Published: (2016)

An inviscid computational study of three '07 Mars lander aeroshell configurations over a Mach number range of 2.3 to 4.5 /
by: Prabhu, Ramadas K.
Published: (2001)

Mach 5 inlet CFD and experimental results /
by: Weir, Lois J.
Published: (1989)

Mach 5 inlet CFD and experimental results /
by: Weir, Lois J.
Published: (1989)

Investigation of materials for boundary layer control in a supersonic wind tunnel /
by: Braafladt, Alexander C., et al.
Published: (2013)

Experimental surface pressure data obtained on 65 ° delta wing across Reynolds number and Mach number ranges /
by: Chu, Julio, et al.
Published: (1996)

Wind tunnel results of the aerodynamic performance of a 1/8-scale model of a twin-engine transport with multi-element wing /
by: Laflin, Brenda E. Gile, et al.
Published: (1997)

Analysis of buzz in a supersonic inlet /
by: Chima, Rodrick V.
Published: (2012)

Experimental aeroheating study in NASA LaRC 20-Inch Mach 6 air tunnel : discrete roughness on BOLT -- test 7071 /
by: Berry, Scott A., et al.
Published: (2023)

Study of the integration of wind tunnel and computational methods for aerodynamic configurations /
by: Browne, Lindsay E.
Published: (1989)

Research on supersonic inlet bleed /
by: Davis, David O.
Published: (2012)

A wind tunnel investigation of three NACA 1-series inlets at Mach numbers up to 0.92 /
by: Re, Richard J., et al.
Published: (1996)

Experimental measurements of sonic boom signatures using a continuous data acquisition technique /
by: Wilcox, Floyd J. (Floyd Jay)
Published: (2013)

Wind tunnel simulations of aeolian processes /
by: Greeley, Ronald
Published: (1984)

Freestream Mach-number and temperature measurement in NASA Langley's 20-inch supersonic wind tunnel using laser-induced thermal acoustics /
by: Herring, Gregory C., et al.
Published: (2020)

Numerical simulation of scramjet inlet flow fields /
by: Kumar, Ajay
Published: (1986)

Design and calibration of the mixing layer and wind tunnel /
by: Bell, James H.
Published: (1989)

Experimental investigation of Mars Science Laboratory entry vehicle aeroheating in AEDC hypervelocity tunnel 9 /
by: Hollis, Brian R. (Brian Ray), et al.
Published: (2017)

Summary of the 2017 blockage test in the 10- by 10-foot supersonic wind tunnel /
by: Pastor-Barsi, Christine, 1982-, et al.
Published: (2018)

Experimental study of boundary layer behavior in a simulated low pressure turbine /
by: Shyne, Rickey J.
Published: (1998)

Two-dimensional wind tunnel.
Published: (1982)

CFD simulations for the effect of unsteady wakes on the boundary layer of a highly loaded low-pressure turbine airfoil (L1A), final report /
by: Vinci, Samuel J.
Published: (2012)

Investigation of solid plume simulation criteria to produce flight plume effects on multibody configuration in wind tunnel tests /
by: Frost, Alonzo L.
Published: (1986)

FORTRAN programs for calculating wind-tunnel boundary interference /
by: Heyson, Harry H.
Published: (1969)

Wind tunnel evaluation of airfoil performance using simulated ice shapes /
by: Bragg, Michael B., 1954-
Published: (1982)

Computational fluid dynamics (CFD) simulation of hypersonic turbine-based combined-cycle (TBCC) inlet mode transition /
by: Slater, John W.
Published: (2010)

Investigation of active flow control to improve aerodynamic performance of oscillating wings /
by: Narducci, Robert P.
Published: (2014)

The NASA Langley 16-foot transonic tunnel : historical overview, facility description, calibration, flow characteristics, and test capabilities /
Published: (1995)

Hot-bench simulation of the active flexible wing wind-tunnel model /
by: Buttrill, Carey S.
Published: (1990)

Role of computational fluid dynamics and wind tunnels in aeronautics R&D /
Published: (2012)

Wind tunnel interference effects on tiltrotor testing using computational fluid dynamics /
by: Koning, Witold J. F.
Published: (2016)

Wind tunnel test of a risk-reduction wing/fuselage model to examine juncture-flow phenomena /
by: Kegerise, Michael A., et al.
Published: (2016)

Development of microchannel plates in advanced wind-tunnel instrumentation /
by: Feller, W. Bruce
Published: (1990)

Flow unsteadiness effects on boundary layers /
by: Murthy, Sreedhara V.
Published: (1989)