[PDF] A Comparison Of The Performance Of Four Side Mounted Inlets Over A Mach Number Range Of 088 To 22 And Angles Of Attack To 14 eBook

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Preliminary Investigation of Shield to Improve Angle-of-attack Performance of Nacelle-type Inlet

Milton A. Beheim
Preliminary Investigation of Shield to Improve Angle-of-attack Performance of Nacelle-type Inlet by Milton A. Beheim PDF

Author : Milton A. Beheim
Publisher :
Page : 38 pages
File Size : 46,53 MB
Release : 1957
Category : Airplanes
ISBN :

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An investigation was conducted at Mach numbers between 1.6 and 2.0 on the use of a shield along the upper-half periphery of the cowl of a conical inlet to improve performance at angle of attack. The best results were obtained with the shield mounted in such a manner that an air gap existed between the shield and the cowl lip. Zero-angle-of-attack performance was not appreciably affected. At an angle of attack of 8 degrees distortion was about half that without the shield, and subcritical stability was improved.