Author: Bruce Boguski
Publisher:
ISBN: 9781931588003
Category : Education
Languages : en
Pages : 172
Book Description
The Testing Zone
Author: Bruce Boguski
Publisher:
ISBN: 9781931588003
Category : Education
Languages : en
Pages : 172
Book Description
Publisher:
ISBN: 9781931588003
Category : Education
Languages : en
Pages : 172
Book Description
Methodology, Results, and Significance of an Unsaturated-zone Tracer Test at an Artificial-recharge Facility, Tucson, Arizona
Author: D. D. Graham
Publisher:
ISBN:
Category : Artificial groundwater recharge
Languages : en
Pages : 36
Book Description
Publisher:
ISBN:
Category : Artificial groundwater recharge
Languages : en
Pages : 36
Book Description
Pittsburgh Area Transportation Study
Shore Zone Land Use and Land Cover: Central Atlantic Regional Ecological Test Site
Author: Robert Dolan
Publisher:
ISBN:
Category : Coastal ecology
Languages : en
Pages : 64
Book Description
Publisher:
ISBN:
Category : Coastal ecology
Languages : en
Pages : 64
Book Description
Report of the Tests of Metals and Other Materials for Industrial Purposes
Author: United States. Army. Ordnance Department
Publisher:
ISBN:
Category : Materials
Languages : en
Pages : 644
Book Description
Publisher:
ISBN:
Category : Materials
Languages : en
Pages : 644
Book Description
Water-resources Investigations Report
Railway Signaling and Communications
Results of a 0.2-scale B-1 Inlet Verification Model Test at Transonic and Supersonic Mach Numbers
Author: John F. Riddell
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 250
Book Description
Results are presented of a wind tunnel investigation of a 0.2-scale model of the left-hand dual-inlet air induction system of the B-1 aircraft. The test was conducted at Mach numbers from 0.55 to 2.3 over an angle-of-attack range from -2 to 13 deg and yaw angles of -6 to 6 deg. Inlet performance in terms of compressor-face total-pressure recovery, total-pressure distortion and turbulence index is presented as a function of engine-face mass-flow ratio for various inlet geometries and model attitudes. Generally, increasing angle of attack caused greated decreases in the performance of the inboard inlet at supersonic Mach numbers and of the outboard inlet at subsonic Mach numbers. Noticeable effects occurred when the structural mode control vanes were varied at the subsonic Mach number at low angles of attack and at negative yaw. (Author).
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 250
Book Description
Results are presented of a wind tunnel investigation of a 0.2-scale model of the left-hand dual-inlet air induction system of the B-1 aircraft. The test was conducted at Mach numbers from 0.55 to 2.3 over an angle-of-attack range from -2 to 13 deg and yaw angles of -6 to 6 deg. Inlet performance in terms of compressor-face total-pressure recovery, total-pressure distortion and turbulence index is presented as a function of engine-face mass-flow ratio for various inlet geometries and model attitudes. Generally, increasing angle of attack caused greated decreases in the performance of the inboard inlet at supersonic Mach numbers and of the outboard inlet at subsonic Mach numbers. Noticeable effects occurred when the structural mode control vanes were varied at the subsonic Mach number at low angles of attack and at negative yaw. (Author).
Research Conference on Shear Strength of Cohesive Soils; Sponsored by the Soil Mechanics and Foundations Division, ASCE. [Papers and Reports
Author:
Publisher:
ISBN:
Category : Soil mechanics
Languages : en
Pages : 1190
Book Description
Publisher:
ISBN:
Category : Soil mechanics
Languages : en
Pages : 1190
Book Description