Abnormal Peaks Of Increased Heat Transfer On The Blunted Delta Wing In The Hypersonic Flow
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An Experimental Study of the Pressure and Heat-transfer Distribution on a 70° Sweep Slab Delta Wing in Hypersonic Flow
Author | : Mitchel H. Bertram |
Publisher | : |
Total Pages | : 134 |
Release | : 1963 |
Genre | : Airplanes |
ISBN | : |
Analysis of Hypersonic Pressure and Heat Transfer Tests on Delta Wings with Laminar and Turbulent Boundary Layers
Author | : A. L. Nagel |
Publisher | : |
Total Pages | : 206 |
Release | : 1966 |
Genre | : Aerodynamics, Hypersonic |
ISBN | : |
The High Temperature Aspects of Hypersonic Flow
Author | : Wilbur C. Nelson |
Publisher | : Elsevier |
Total Pages | : 801 |
Release | : 2014-12-02 |
Genre | : Science |
ISBN | : 1483223310 |
The High Temperature Aspects of Hypersonic Flow is a record of the proceedings of the AGARD-NATO Specialists' Meeting, held at the Technical Centre for Experimental Aerodynamics, Rhode-Saint-Genese, Belgium in April 1962. The book contains the papers presented during the meeting that tackled a broad range of topics in the aspects of hypersonic flow. The subjects covered during the meeting include pressure measurements, interference effects, the use of wind tunnels in aircraft development testing, high temperature gas characteristics, boundary layer research, stability and control and the use of rocket vehicles in flight research. Aerospace engineers and aeronautical engineers will find the book invaluable.
Pressures and Heat Transfer on a 75 ̊swept Delta Wing with Trailing-edge Flap at Mach 6 and Angles of Attack to 90
Author | : J. Wayne Keyes |
Publisher | : |
Total Pages | : 52 |
Release | : 1969 |
Genre | : Aerodynamic heating |
ISBN | : |
Pressure and heat transfer on swept delta wing with trailing-edge flap.
On the Hypersonic Flow Past Blunted, Flat Delta Wings
Author | : Arnold Polak |
Publisher | : |
Total Pages | : 48 |
Release | : 1970 |
Genre | : Aerodynamics, Hypersonic |
ISBN | : |
The flow of a perfect gas over the slab portion of a blunted delta wing flying at hypersonic speeds is studied. A set of approximate equations is derived and a solution - for an inviscid flow - is obtained. Using this solution as a representation for the inviscid flow problem, a formulation to the laminar boundary-layer equations is presented; one which is applicable to the flow field's azimuthal planes where the crossflow gradients are not too large. Numerical solutions to these boundary-layer equations have been obtained; however, these are restricted to the azimuthal planes and near to the leading edges. The results indicate the presence of a dividing surface streamline since a numerical solution could not be obtained near the centerplane of the wing, where the crossflow velocity is large. (Author).
A Study of the Pressure and Heat Transfer Distribution on a Highly Swept Slap Delta Wing in Hypersonic Flow
Author | : Allen Hallett Whitehead |
Publisher | : |
Total Pages | : 152 |
Release | : 1966 |
Genre | : Aerodynamics, Hypersonic |
ISBN | : |