Research on Blunt-faced Entry Configurations at Angles of Attack Between 60° and 90° PDF Download

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Research on Blunt-faced Entry Configurations at Angles of Attack Between 60° and 90°

Research on Blunt-faced Entry Configurations at Angles of Attack Between 60° and 90° PDF Author: William H. Phillips
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 20

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Research on Blunt-faced Entry Configurations at Angles of Attack Between 60° and 90°

Research on Blunt-faced Entry Configurations at Angles of Attack Between 60° and 90° PDF Author: William H. Phillips
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 20

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Book Description

Research on Blunt-faced Entry Configurations at Angles of Attack Between 60 Deg and 90 Deg

Research on Blunt-faced Entry Configurations at Angles of Attack Between 60 Deg and 90 Deg PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 20

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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 : 284

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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.

NASA Scientific and Technical Reports

NASA Scientific and Technical Reports PDF Author: United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1440

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A Selected Listing of NASA Scientific and Technical Reports for ...

A Selected Listing of NASA Scientific and Technical Reports for ... PDF Author: United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1680

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Pressure Distributions on Blunt Delta Wings at a Mach Number of 2.91 and Angles of Attack Up to 90 Deg

Pressure Distributions on Blunt Delta Wings at a Mach Number of 2.91 and Angles of Attack Up to 90 Deg PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 120

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Supersonic Aerodynamic Characteristics of Triangular Plan-form Models at Angles of Attack to 90 Degrees

Supersonic Aerodynamic Characteristics of Triangular Plan-form Models at Angles of Attack to 90 Degrees PDF Author:
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ISBN:
Category :
Languages : en
Pages : 46

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Government-wide Index to Federal Research & Development Reports

Government-wide Index to Federal Research & Development Reports PDF Author:
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ISBN:
Category : Government publications
Languages : en
Pages : 1466

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Static Longitudinal Aerodynamic Characteristics at Transonic Speeds of a Lenticular-shaped Reentry Vehicle

Static Longitudinal Aerodynamic Characteristics at Transonic Speeds of a Lenticular-shaped Reentry Vehicle PDF Author: John P. Mugler
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 34

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The Application of Some Lifting-body Reentry Concepts to Missile Design

The Application of Some Lifting-body Reentry Concepts to Missile Design PDF Author: M. Leroy Spearman
Publisher:
ISBN:
Category : Guided missiles
Languages : en
Pages : 34

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