Investigation of the Static Longitudinal Stability Characteristics of an Air-to-surface Canard Missile Configuration in the Transonic Mach Number Range PDF Download

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Investigation of the Static Longitudinal Stability Characteristics of an Air-to-surface Canard Missile Configuration in the Transonic Mach Number Range

Investigation of the Static Longitudinal Stability Characteristics of an Air-to-surface Canard Missile Configuration in the Transonic Mach Number Range PDF Author: Gerald L. Hunt
Publisher:
ISBN:
Category : Air-to-surface missiles
Languages : en
Pages : 24

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Book Description

Investigation of the Static Longitudinal Stability Characteristics of an Air-to-surface Canard Missile Configuration in the Transonic Mach Number Range

Investigation of the Static Longitudinal Stability Characteristics of an Air-to-surface Canard Missile Configuration in the Transonic Mach Number Range PDF Author: Gerald L. Hunt
Publisher:
ISBN:
Category : Air-to-surface missiles
Languages : en
Pages : 24

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Book Description

Longitudinal Stability and Control Characteristics from a Flight Investigation of a Cruciform Canard Missile Configuration Having an Exposed Wing-canard Area Ratio of 16:1

Longitudinal Stability and Control Characteristics from a Flight Investigation of a Cruciform Canard Missile Configuration Having an Exposed Wing-canard Area Ratio of 16:1 PDF Author: Martin T. Moul
Publisher:
ISBN:
Category : Rockets (Aeronautics)
Languages : en
Pages : 42

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Book Description

Investigation of the Static Longitudinal Stability and Roll Characteristics of a Three-stage Missile Configuration at Mach Numbers from 1.77 to 2.87

Investigation of the Static Longitudinal Stability and Roll Characteristics of a Three-stage Missile Configuration at Mach Numbers from 1.77 to 2.87 PDF Author: Donald T. Gregory
Publisher:
ISBN:
Category : Stability of airplanes, Longitudinal
Languages : en
Pages : 36

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Book Description

Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 648

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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.

Preliminary Investigation of the Effects of Several Seeker-nose Configurations on the Longitudinal Characteristics of a Canard-type Missile at a Mach Number of 1.60

Preliminary Investigation of the Effects of Several Seeker-nose Configurations on the Longitudinal Characteristics of a Canard-type Missile at a Mach Number of 1.60 PDF Author: A. Warner Robins
Publisher:
ISBN:
Category : Rockets (Aeronautics)
Languages : en
Pages : 32

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Book Description

Flight Investigation at Low Angles of Attack to Determine the Longitudinal Stability and Control Characteristics of a Cruciform Canard Missile Configuration with a Low-aspect-ratio Wing and Blunt Nose at Mach Numbers from 1.2 to 2.1

Flight Investigation at Low Angles of Attack to Determine the Longitudinal Stability and Control Characteristics of a Cruciform Canard Missile Configuration with a Low-aspect-ratio Wing and Blunt Nose at Mach Numbers from 1.2 to 2.1 PDF Author: Clarence A. Brown
Publisher:
ISBN:
Category : Charts, diagrams, etc
Languages : en
Pages : 37

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Book Description
A full-scale rocket-powered model of a cruciform canard missile configuration with a low-aspect ratio wing and blunt nose has been flight tested by the Langley Pilotless Aircraft Research Division. Static and dynamic longitudinal stability and control derivatives of this interdigitated canard-wing missile configuration were determined by using the pulsed-control technique at low angles of attack and for a Mach number range of 1.2 to 2.1.

Three-degree-of-freedom Evaluation of the Longitudinal Transfer Functions of a Supersonic Canard Missile Configuration Including Changes in Forward Speed

Three-degree-of-freedom Evaluation of the Longitudinal Transfer Functions of a Supersonic Canard Missile Configuration Including Changes in Forward Speed PDF Author: Ernest C. Seaberg
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 36

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Book Description
A reevaluation of existing flight data obtained for a supersonic canard missile configuration of the boost-glide type has been made to determine derivatives not previously evaluated. These derivatives, together with those previously evaluated and published, have been utilized to determine some typical airframe frequency responses based on the three-degree-of-freedom longitudinal equations of motion.

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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Book Description

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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Book Description

Aerodynamic Characteristics at Mach Numbers from 1.50 to 4.63 of a Maneuverable Missile with In-line Cruciform Wings and Canard Surfaces

Aerodynamic Characteristics at Mach Numbers from 1.50 to 4.63 of a Maneuverable Missile with In-line Cruciform Wings and Canard Surfaces PDF Author: M. Leroy Spearman
Publisher:
ISBN:
Category : Guided missiles
Languages : en
Pages : 52

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Book Description
An investigation has been conducted in the Langley Unitary Plan wind tunnel at Mach numbers from 1.50 to 4.63 to determine the aerodynamic characteristics of a maneuverable missile having in-line cruciform wings and canard surfaces oriented in 45° roll planes.