Add to ORKGUnsteady pressure distributions measured in a transonic wind tunnel on a supercritical airfoil of 13% maximum thickness with an oscillating trailing edge flap were analyzed. The influences of oscillation frequency, flap mean deflection, and incidence on the unsteady pressure distribution are discussed in the Mach number range of 0.3 to 0.85; the effects of the oscillation amplitude at M = 0.78 are also analyzed. Unsteady lift and moment coefficients obtained from unsteady pressure distributions are discussed
This paper reports about our experimental and numerical investigations of forced and self-sustained ...
The experiments described, in conjunction with an earlier study by the author, comprise a set which ...
In the Transonic Wind tunnel Göttingen, different test campaigns were performed with an oscillating ...
Unsteady pressure distributions measured in a transonic wind tunnel on a supercritical airfoil of 13...
With 35 figs., 2 tabs. and 13 refs.Copy held by FIZ Karlsruhe; available from UB/TIB Hannover / FIZ ...
Exploratory wind-tunnel experiments in high-subsonic and transonic flow on a conventional airfoil wi...
We present experimental and numerical investigations of steady and unsteady transonic flow past a 2-...
Exploratory wind-tunnel experiments in high-subsonic and transonic flow on a conventional airfoil wi...
As Part of a Multi-Phased Research Program, Known as the Benchmark Models Program, at the NASA Langl...
As Part of a Multi-Phased Research Program, Known as the Benchmark Models Program, at the NASA Langl...
In the Transonic Wind Tunnel Goettingen, pitch oscillations were performed with a Lambda wing to stu...
An extensive set of unsteady pressure data was acquired along the midspan of a modern transonic fan ...
The experimental results of steady and unsteady pressure measurements, carried out in subsonic and t...
In the frame work of the JAXA-DLR cooperation, wind tunnel test for measuring unsteady aerodynamics ...
(Maximum 200 words) Transonic steady- and unsteady-pressure tests have been conducted on a large el...
This paper reports about our experimental and numerical investigations of forced and self-sustained ...
The experiments described, in conjunction with an earlier study by the author, comprise a set which ...
In the Transonic Wind tunnel Göttingen, different test campaigns were performed with an oscillating ...
Unsteady pressure distributions measured in a transonic wind tunnel on a supercritical airfoil of 13...
With 35 figs., 2 tabs. and 13 refs.Copy held by FIZ Karlsruhe; available from UB/TIB Hannover / FIZ ...
Exploratory wind-tunnel experiments in high-subsonic and transonic flow on a conventional airfoil wi...
We present experimental and numerical investigations of steady and unsteady transonic flow past a 2-...
Exploratory wind-tunnel experiments in high-subsonic and transonic flow on a conventional airfoil wi...
As Part of a Multi-Phased Research Program, Known as the Benchmark Models Program, at the NASA Langl...
As Part of a Multi-Phased Research Program, Known as the Benchmark Models Program, at the NASA Langl...
In the Transonic Wind Tunnel Goettingen, pitch oscillations were performed with a Lambda wing to stu...
An extensive set of unsteady pressure data was acquired along the midspan of a modern transonic fan ...
The experimental results of steady and unsteady pressure measurements, carried out in subsonic and t...
In the frame work of the JAXA-DLR cooperation, wind tunnel test for measuring unsteady aerodynamics ...
(Maximum 200 words) Transonic steady- and unsteady-pressure tests have been conducted on a large el...
This paper reports about our experimental and numerical investigations of forced and self-sustained ...
The experiments described, in conjunction with an earlier study by the author, comprise a set which ...
In the Transonic Wind tunnel Göttingen, different test campaigns were performed with an oscillating ...