Experimental Aerodynamic Characteristics for a Cylindrical Body of Revolution with Various Noses at Angles of Attack from 0 ̊to 58 ̊and Mach Numbers from 0.6 to 2.0

Experimental Aerodynamic Characteristics for a Cylindrical Body of Revolution with Various Noses at Angles of Attack from 0 ̊to 58 ̊and Mach Numbers from 0.6 to 2.0 PDF Author: Leland Howard Jorgensen
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ISBN:
Category : Aerodynamics
Languages : en
Pages : 100

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Experimental Aerodynamic Characteristics for a Cylindrical Body of Revolution with Side Strakes and Various Noses at Angles of Attack from 0 ̊to 58 ̊and Mach Numbers from 0.6 to 2.0

Experimental Aerodynamic Characteristics for a Cylindrical Body of Revolution with Side Strakes and Various Noses at Angles of Attack from 0 ̊to 58 ̊and Mach Numbers from 0.6 to 2.0 PDF Author: Leland H. Jorgensen
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 122

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Induced Side Forces on Bodies of Revolution at High Angle of Attack

Induced Side Forces on Bodies of Revolution at High Angle of Attack PDF Author: Wardlaw, Jr. (Andrew B.)
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ISBN:
Category : Aerodynamic load
Languages : en
Pages : 52

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Linear regression techniques are used to establish a quantitative description of side forces on bodies at high incidence. A data base is assembled concerning the key side force characteristics of maximum observed side force, angle of occurrence, and minimum angle of attack at which a side force is observed. This information is examined to determine the important trends and a predictive model for side force based on the crossflow analogy is developed to suggest other important variables. A linear regression model for these quantities is developed to include only those variables which are statistically significant. Results indicate that peak side force coefficients are a function of Mach number and only weakly of Reynolds number. Nose fineness is the critical model dimension which suggests that peak side force is a product of the nose flow field. The angle at which peak side forces occur is found to be dependent on model length and Mach number, while the onset angle of attack is a function of model length only.

NASA Technical Report

NASA Technical Report PDF Author:
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ISBN:
Category : Aerodynamics
Languages : en
Pages : 470

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Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
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ISBN:
Category : Aeronautics
Languages : en
Pages : 1074

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NASA Technical Memorandum

NASA Technical Memorandum PDF Author:
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ISBN:
Category : Aeronautics
Languages : en
Pages : 104

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Prediction of Static Aerodynamic Characteristics for Slender Bodies Alone and with Lifting Surfaces to Very High Angles of Attack

Prediction of Static Aerodynamic Characteristics for Slender Bodies Alone and with Lifting Surfaces to Very High Angles of Attack PDF Author: Leland Howard Jorgensen
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 254

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Prediction of Static Aerodynamic Characteristics for Slender Bodies Alone and with Lifting Surfaces to Very High Angles of Attack

Prediction of Static Aerodynamic Characteristics for Slender Bodies Alone and with Lifting Surfaces to Very High Angles of Attack PDF Author: Leland H. Jorgensen
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 248

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Government Reports Annual Index

Government Reports Annual Index PDF Author:
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ISBN:
Category : Government reports announcements & index
Languages : en
Pages : 882

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Index to NASA Technical Publications

Index to NASA Technical Publications PDF Author: United States. National Aeronautics and Space Administration
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Category :
Languages : en
Pages :

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