Mach Number

136 books
NASA Glenn 1-by 1-foot supersonic wind tunnel user manualUnknown Author

NASA Glenn 1-by 1-foot supersonic wind tunnel user manual

Unknown Author

1999No page data
In-flight transition measurement on a 10David F. Fisher
⏱ 2h 20m

In-flight transition measurement on a 10

David F. Fisher

1982140 pp.
In-flight transition measurement on a 10p0s cone at Mach numbers from 0.5 to 2.0David F Fisher
⏱ 2h 20m

In-flight transition measurement on a 10p0s cone at Mach numbers from 0.5 to 2.0

David F Fisher

1982140 pp.
NACA mach number warning device for use in flightLangley Aeronautical Laboratory
⏱ 20m

NACA mach number warning device for use in flight

Langley Aeronautical Laboratory

194420 pp.
Behavior of fast moving flow of compressible gas in cylindrical pipe in presence of coolingUnited States.: National Advisory Committee for Aeronautics
⏱ 16m

Behavior of fast moving flow of compressible gas in cylindrical pipe in presence of cooling

United States.: National Advisory Committee for Aeronautics

195116 pp.
The influence of Mach number and heat transfer on the turbulent flow wall lawJulius Rotta

The influence of Mach number and heat transfer on the turbulent flow wall law

Julius Rotta

1988No page data
Highlights of unsteady pressure tests on a 14 percent supercritical airfoil at high Reynolds number, transonic conditionUnknown Author

Highlights of unsteady pressure tests on a 14 percent supercritical airfoil at high Reynolds number, transonic condition

Unknown Author

1987No page data
Effects of independent variation of Mach and Reynolds numbers on the low-speed aerodynamic characteristics of the NACA 0012 airfoil sectionCharles L. Ladson

Effects of independent variation of Mach and Reynolds numbers on the low-speed aerodynamic characteristics of the NACA 0012 airfoil section

Charles L. Ladson

1988No page data
Mach number measurements in high-speed wind tunnelsJacques A. F. Hill
⏱ 1h 53m

Mach number measurements in high-speed wind tunnels

Jacques A. F. Hill

1956113 pp.
Flow of a compressible fluid past a circular arc profileLangley Aeronautical Laboratory
⏱ 2h 2m

Flow of a compressible fluid past a circular arc profile

Langley Aeronautical Laboratory

1944122 pp.
Sphere drag at high Knudsen number and low Mach numberD. Roger Willis
⏱ 19m

Sphere drag at high Knudsen number and low Mach number

D. Roger Willis

196519 pp.
Flight and wind-tunnel measurements showing base drag reduction provided by a trailing disk for high Reynolds number turbulent flow for subsonic and transonic Mach numbersSheryll Goecke Powers

Flight and wind-tunnel measurements showing base drag reduction provided by a trailing disk for high Reynolds number turbulent flow for subsonic and transonic Mach numbers

Sheryll Goecke Powers

1988No page data
Experimental evaluation of wall Mach number distributions of the octagonal test section proposed for NASA Lewis Research Center's altitude wind tunnelDouglas E. Harrington

Experimental evaluation of wall Mach number distributions of the octagonal test section proposed for NASA Lewis Research Center's altitude wind tunnel

Douglas E. Harrington

1986No page data
Comparison of experimental surface pressure with theoretical predictions on twin two-dimensional convergent-divergent nozzlesJohn R. Carlson

Comparison of experimental surface pressure with theoretical predictions on twin two-dimensional convergent-divergent nozzles

John R. Carlson

1986No page data
Flow-separation patterns on symmetric forebodiesEarl R. Keener
⏱ 2h 15m

Flow-separation patterns on symmetric forebodies

Earl R. Keener

1986135 pp.
High-resolution shock capturing scheme for high Mach number internal flowSeokkwan Yoon

High-resolution shock capturing scheme for high Mach number internal flow

Seokkwan Yoon

1986No page data
Effect of Reynolds number and Mach number on flow angularity probe sensitivityLeigh Ann Smith

Effect of Reynolds number and Mach number on flow angularity probe sensitivity

Leigh Ann Smith

1986No page data
Turbulent skin friction at high Mach numbers and Reynolds numbers in air and heliumFred W. Matting
⏱ 39m

Turbulent skin friction at high Mach numbers and Reynolds numbers in air and helium

Fred W. Matting

196139 pp.
Full flight envelope direct thrust measurement on a supersonic aircraftTimothy R. Conners

Full flight envelope direct thrust measurement on a supersonic aircraft

Timothy R. Conners

1998No page data
Progress in Favré-Reynolds stress closures for compressible flowsV. Adumitroaie

Progress in Favré-Reynolds stress closures for compressible flows

V. Adumitroaie

1998No page data
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