Performance Characteristics of a Wing-body Combination with a Two-dimensional External-internal-compression Inlet at Mach 3.5 and 3.0 PDF Download

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Performance Characteristics of a Wing-body Combination with a Two-dimensional External-internal-compression Inlet at Mach 3.5 and 3.0

Performance Characteristics of a Wing-body Combination with a Two-dimensional External-internal-compression Inlet at Mach 3.5 and 3.0 PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 38

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Performance Characteristics of a Wing-body Combination with a Two-dimensional External-internal-compression Inlet at Mach 3.5 and 3.0

Performance Characteristics of a Wing-body Combination with a Two-dimensional External-internal-compression Inlet at Mach 3.5 and 3.0 PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 38

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Book Description

The Effect on the Drag of a Wing-body Combination of Moment-of-area-rule Modifications with Pods Ducted to Simulate Engine Nacelles

The Effect on the Drag of a Wing-body Combination of Moment-of-area-rule Modifications with Pods Ducted to Simulate Engine Nacelles PDF Author: Robert R. Dickey
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 24

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Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 758

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Book Description
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.

Longitudinal Aerodynamic Characteristics at Mach Number 2.02 of a Series of Wing-body Configurations Employing a Cambered and Twisted Arrow Wing

Longitudinal Aerodynamic Characteristics at Mach Number 2.02 of a Series of Wing-body Configurations Employing a Cambered and Twisted Arrow Wing PDF Author: Harry W. Carlson
Publisher:
ISBN:
Category :
Languages : en
Pages : 20

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Keywords Index to U.S. Government Technical Reports

Keywords Index to U.S. Government Technical Reports PDF Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1160

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Keywords Index to U.S. Government Technical Reports (permuted Title Index).

Keywords Index to U.S. Government Technical Reports (permuted Title Index). PDF Author: United States. Department of Commerce. Office of Technical Services
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 836

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Performance of a Mach 3.0 Design Axisymmetric Double-cone External-compression Inlet in the Mach Number Range of 1.97 to 0.79

Performance of a Mach 3.0 Design Axisymmetric Double-cone External-compression Inlet in the Mach Number Range of 1.97 to 0.79 PDF Author: Owen H. Davis
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 29

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Experimental Pressure Distributions Over Two Wing-body Combinations at Mach Number 1.9

Experimental Pressure Distributions Over Two Wing-body Combinations at Mach Number 1.9 PDF Author: Barry Moskowitz
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 40

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Book Description
Abstract: Pressure distributions on two wing-body combinations were obtained at Mach number of 1.9 to investigate wing-body interference. A rectangular wing, a triangular wing, and a cylindrical body having an ogive nose were investigated alone and in combination. Pressure distributions over the wing body combination compared favorable with theoretical calculations based primarily on a generalization of the method of Nielsen and Matteson, except at the root section of wings where boundary layer of body modified the flow.

A Transonic Investigation of Changing Indentation Design Mach Number on the Aerodynamic Characteristics of a 45 Degree Sweptback-wing-body Combination Designed for High Performance

A Transonic Investigation of Changing Indentation Design Mach Number on the Aerodynamic Characteristics of a 45 Degree Sweptback-wing-body Combination Designed for High Performance PDF Author: Donald L. Loving
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 92

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Effects of Wing Planform on the Aerodynamic Characteristics of a Wing-body-tail Model at Mach Numbers 1.57, 2.16, and 2.87

Effects of Wing Planform on the Aerodynamic Characteristics of a Wing-body-tail Model at Mach Numbers 1.57, 2.16, and 2.87 PDF Author: Royce L. McKinney
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 52

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Book Description