Flight Determination of Drag and Pressure Recovery of Two Scoop Inlets Located at Maximum-body-diameter Station at Mach Numbers from 0.8 to 1.8

Flight Determination of Drag and Pressure Recovery of Two Scoop Inlets Located at Maximum-body-diameter Station at Mach Numbers from 0.8 to 1.8
Author: Leonard W. Putland
Publisher:
Total Pages: 30
Release: 1956
Genre: Boundary layer control
ISBN:

Two models each utilizing a scoop inlet located at the maximum-body-diameter station operating mass-flow ratios from 0.76 to 0.96 have been flight tested at an angle of attack of approximately zero degrees over a Mach number range from 0.8 to 1.8, and a Reynolds number range from 2,000,000 to7,000,000 based on body maximum diameter. One of the scoop inlets had a circular cross section with a boundary-layer diverter. The other scoop inlet had a semicircular cross section wrapped partly around the body with a boundary-layer splitter plate ahead of the inlet.

Preliminary Flight Measurements of the Total Pressure Recovery of a Split-Wing Ram-Jet Inlet at Mach Numbers from 1. 4 To 3. 16

Preliminary Flight Measurements of the Total Pressure Recovery of a Split-Wing Ram-Jet Inlet at Mach Numbers from 1. 4 To 3. 16
Author: A. H. Hinners
Publisher: BiblioGov
Total Pages: 32
Release: 2013-07
Genre:
ISBN: 9781289267643

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