An experimental approach to a rapid propulsion and aeronautics concepts testbed /

Supersonic wind tunnel tests of a half-axisymmetric 12°-spike inlet to a rocket-based combined-cycle propulsion system /
by: DeBonis, James R., et al.
Published: (2001)

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

Experimental and computational sonic boom assessment of Boeing N+2 low boom models /
by: Durston, D. A.
Published: (2015)

Mid-fidelity computational fluid dynamics analysis of the Elytron 4S UAV concept /
by: Koning, Witold J. F.
Published: (2018)

Fundamental ice crystal accretion physics studies /
Published: (2012)

Evaluation of the low-speed stability and control characteristics of a Mach 5.5 Waverider concept /
by: Hahne, David E. (David Edgar)
Published: (1997)

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)

Flow quality survey of the 8-by 6-foot supersonic wind tunnel (2015 test) prior to the 9-by 15-foot low-speed wind tunnel acoustic improvement modifications /
by: Johnson, Aaron M.
Published: (2018)

Rotor CFD analysis at terrestrial and martian atmospheric densities /
by: Perez Perez, Brenda Natalia
Published: (2018)

Review of the Aerodynamic Acceptance Test and application to anti-icing fluids testing in the NRC propulsion and icing wind tunnel /
by: Broeren, Andy P., et al.
Published: (2012)

Experimental studies of transonic flow field near a longitudinally slotted wind tunnel wall /
by: Everhart, Joel L.
Published: (1994)

1-by 1- foot supersonic wind tunnel sidewall flowfield compression plate study /
by: Peters, Christopher J. (Christopher John), et al.
Published: (2020)

Mars tumbleweed : FY2003 conceptual design assessment /
Published: (2005)

Experimental aeroelasticity history, status and future in brief /
by: Ricketts, Rodney H.
Published: (1990)

Aerodynamic measurements on a large splitter plate for the NASA Langley Transonic Dynamics Tunnel /
by: Schuster, D. M. (David M.)
Published: (2001)

Pressure probe designs for dynamic pressure measurements in a supersonic flow field /
by: Porro, A. Robert
Published: (2001)

Aerodynamic measurements on a large splitter plate for the NASA Langley Transonic Dynamics Tunnel /
by: Schuster, D. M. (David M.)
Published: (2001)

A two-dimensional adaptive-wall test section with ventilated walls in the Ames 2- by 2-foot transonic wind tunnel /
by: Schairer, Edward T.
Published: (1989)

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

Rime ice accretion and its effect on airfoil performance /
by: Bragg, Michael B., 1954-
Published: (1982)

Mach 5 to 7 RBCC propulsion system testing at NASA-LeRC HTF /
by: Perkins, H. Douglas, et al.
Published: (1996)

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)

Experimental investigation of hexcomb-pattern roughness effects on transition onset and turbulent heating augmentation at Mach 6 /
by: Hollis, Brian R. (Brian Ray)
Published: (2019)

Flight, wind-tunnel, and computational fluid dynamics comparison for cranked arrow wing (F-16XL-1) at subsonic and transonic speeds /
Published: (2001)

Two-dimensional wind tunnel.
Published: (1982)

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

Wind-tunnel investigation of a flush airdata system at Mach numbers from 0.7 to 1.4 /
by: Larson, Terry J.
Published: (1990)

NASA Ames Laminar Flow Supersonic Wind Tunnel (LFSWT) tests of a 10 ̊cone at Mach 1.6 /
by: Wolf, Stephen W. D., et al.
Published: (1997)

Subsonic and transonic pressure measurements on a high-aspect-ratio supercritical-wing model with oscillating control surfaces /
by: Sandford, M. C. (Maynard C.)
Published: (1981)

Aero-heating of shallow cavities in hypersonic freestream flow /
Published: (2010)

Modifications to the 4 x 7 meter tunnel for acoustic research : engineering feasibility study.
Published: (1986)

Results of the AFRSI rewaterproofing systems screening test in the NASA/AMES Research Center (ARC) 2x2-foot transonic wind tunnel (OS-310) /
by: Marroquin, J., et al.
Published: (1985)

Comparison of X-31 flight and ground-based yawing moment asymmetries at high angles of attack /
by: Cobleigh, Brent R., et al.
Published: (2001)

Comparison of X-31 flight and ground-based yawing moment asymmetries at high angles of attack /
by: Cobleigh, Brent R.
Published: (2001)

Wind tunnel model design for the study of plume effects on sonic boom for isolated exhaust nozzles /
by: Castner, Raymond S.
Published: (2010)