Static Aerodynamic Characteristics of a Short Blunt 10 Degree Semivertex Angle Cone at a Mach Number of 15 in Helium PDF Download

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Static Aerodynamic Characteristics of a Short Blunt 10 Degree Semivertex Angle Cone at a Mach Number of 15 in Helium

Static Aerodynamic Characteristics of a Short Blunt 10 Degree Semivertex Angle Cone at a Mach Number of 15 in Helium PDF Author: Melvin J. Fohrman
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 48

Book Description


Static Aerodynamic Characteristics of a Short Blunt 10 Degree Semivertex Angle Cone at a Mach Number of 15 in Helium

Static Aerodynamic Characteristics of a Short Blunt 10 Degree Semivertex Angle Cone at a Mach Number of 15 in Helium PDF Author: Melvin J. Fohrman
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 48

Book Description


Longitudinal Aerodynamic Characteristics of Blunted Cones at Mach Numbers of 3.5, 4.2, and 6.0

Longitudinal Aerodynamic Characteristics of Blunted Cones at Mach Numbers of 3.5, 4.2, and 6.0 PDF Author: J. Wayne Keyes
Publisher:
ISBN:
Category : Cone
Languages : en
Pages : 72

Book Description


NASA Technical Note

NASA Technical Note PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 542

Book Description


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 : 258

Book Description


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 : 262

Book Description


NASA Technical Memorandum

NASA Technical Memorandum PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 296

Book Description


Equations and Charts for the Evaluation of the Hypersonic Aerodynamic Characteristics of Lifting Configurations by the Newtonian Theory

Equations and Charts for the Evaluation of the Hypersonic Aerodynamic Characteristics of Lifting Configurations by the Newtonian Theory PDF Author: E. L. Clark
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 98

Book Description
The pressure distribution predicted by the modified Newtonian theory is used to develop equations for the aerodynamic forces, moments, and stability derivatives for components of hypersonic lifting configurations. In conjunction with the equations, a set of charts is presented to enable simple determination of the aerodynamic characteristics of swept cylinders, swept wedges, spherical segments, and cone frustums at zero sideslip and angles of attack from 0 to 180 degrees. This method allows evaluation of most delta wing-body combinations without the need for numerical or graphical integration. As an example of the procedure, the theoretical characteristics of a blunt 75-degree swept delta wing are calculated and compared with experimental results.

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

Book Description


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

Book Description


A Selected Listing of Nasa Scientific and Technical Reports for 1963

A Selected Listing of Nasa Scientific and Technical Reports for 1963 PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 254

Book Description