This paper reviews the derivation of an equation for scaling response surface modeling experiments. The equation represents the smallest number of data points required to fit a linear regression polynomial so as to achieve certain specified model adequacy criteria. Specific criteria are proposed which simplify an otherwise rather complex equation, generating a practical rule of thumb for the minimum volume of data required to adequately fit a polynomial with a specified number of terms in the model. This equation and the simplified rule of thumb it produces can be applied to minimize the cost of wind tunnel testing
The similitude requirements for the most general test conditions are presented. These similitude req...
To apply the experimental data measured in a wind tunnel for a scaled aircraft to a free-flying mode...
Data from extensive check standard tests of seven measurement processes in three NASA Langley Resear...
The factors that determine data volume requirements in a typical wind tunnel test are identified. It...
This paper addresses some issues with quality assessment and quality assurance in response surface m...
A calibration of a hypersonic wind tunnel has been conducted using formal experiment design techniqu...
A new method is presented that computes a pre{test estimate of the upper bound of the drag coefficie...
Report deals with the methods of constructing aerofoils and all other parts of a model airplane, inc...
Some of the basic concepts are unified that were developed for the problem of finding optimal approx...
In conventional wind tunnels the solid-wall or open-jet test section imposes on the flow field aroun...
Wind tunnel testing is sometimes achieved at reduced scale. Doing so, wind engineers must consider t...
This paper was delivered before the Royal Aeronautical Society as the 1925 Wilbur Wright Memorial le...
Results from the Facility Analysis Verification and Operational Reliability project revealed a criti...
The aerodynamic considerations related to model surface definition are examined with particular emph...
A candidate math model search algorithm was developed at Ames Research Center that determines a reco...
The similitude requirements for the most general test conditions are presented. These similitude req...
To apply the experimental data measured in a wind tunnel for a scaled aircraft to a free-flying mode...
Data from extensive check standard tests of seven measurement processes in three NASA Langley Resear...
The factors that determine data volume requirements in a typical wind tunnel test are identified. It...
This paper addresses some issues with quality assessment and quality assurance in response surface m...
A calibration of a hypersonic wind tunnel has been conducted using formal experiment design techniqu...
A new method is presented that computes a pre{test estimate of the upper bound of the drag coefficie...
Report deals with the methods of constructing aerofoils and all other parts of a model airplane, inc...
Some of the basic concepts are unified that were developed for the problem of finding optimal approx...
In conventional wind tunnels the solid-wall or open-jet test section imposes on the flow field aroun...
Wind tunnel testing is sometimes achieved at reduced scale. Doing so, wind engineers must consider t...
This paper was delivered before the Royal Aeronautical Society as the 1925 Wilbur Wright Memorial le...
Results from the Facility Analysis Verification and Operational Reliability project revealed a criti...
The aerodynamic considerations related to model surface definition are examined with particular emph...
A candidate math model search algorithm was developed at Ames Research Center that determines a reco...
The similitude requirements for the most general test conditions are presented. These similitude req...
To apply the experimental data measured in a wind tunnel for a scaled aircraft to a free-flying mode...
Data from extensive check standard tests of seven measurement processes in three NASA Langley Resear...