A Method for the Calculation of External Lift, Moment, and Pressure Drag of Slender Open-nose Bodies of Revolution at Supersonic Speeds PDF Download

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A Method for the Calculation of External Lift, Moment, and Pressure Drag of Slender Open-nose Bodies of Revolution at Supersonic Speeds

A Method for the Calculation of External Lift, Moment, and Pressure Drag of Slender Open-nose Bodies of Revolution at Supersonic Speeds PDF Author: A. M. Peiser
Publisher:
ISBN:
Category : Aerofoils
Languages : en
Pages : 220

Book Description

A Method for the Calculation of External Lift, Moment, and Pressure Drag of Slender Open-nose Bodies of Revolution at Supersonic Speeds

A Method for the Calculation of External Lift, Moment, and Pressure Drag of Slender Open-nose Bodies of Revolution at Supersonic Speeds PDF Author: A. M. Peiser
Publisher:
ISBN:
Category : Aerofoils
Languages : en
Pages : 220

Book Description

A Method for the Calculation of External Lift, Moment, and Pressure Drag of Slender Open-nose Bodies of Revulution at Supersonic Speeds

A Method for the Calculation of External Lift, Moment, and Pressure Drag of Slender Open-nose Bodies of Revulution at Supersonic Speeds PDF Author: Clinton E. Brown
Publisher:
ISBN:
Category :
Languages : en
Pages : 20

Book Description

NACA Wartime Reports. Series L.

NACA Wartime Reports. Series L. PDF Author: Clinton E. Brown
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 20

Book Description
An approximate method is presented for the calculation of the external lift, moment, and pressure drag of slender open-nose bodies of revolution of supersonic speeds. The lift, moment, and pressure drag of a typical ram-jet body shape are calculated at Mach numbers 1.45, 1.60, 1.75, and 3.00; and the lift and moment results are compared with available experimental data. The agreement of the calculated lift and moment data with the experimental data is excellent. The pressure-drag comparison was not presented because of the uncertainty of the amount of skin-friction drag present in the experimental results.

Report - National Advisory Committee for Aeronautics

Report - National Advisory Committee for Aeronautics PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 752

Book Description

Annual Report - National Advisory Committee for Aeronautics

Annual Report - National Advisory Committee for Aeronautics PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages :

Book Description
Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.

Report

Report PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 22

Book Description

Linearized Theory of Steady High-Speed Flow

Linearized Theory of Steady High-Speed Flow PDF Author: G. N. Ward
Publisher: Cambridge University Press
ISBN: 1316601897
Category : Mathematics
Languages : en
Pages : 261

Book Description
Originally published in 1955, this book is devoted exclusively to the problems involved in solving the non-linear equations of motion for compressible fluids.

linearized theory of steady high-speed flow

linearized theory of steady high-speed flow PDF Author:
Publisher: CUP Archive
ISBN:
Category :
Languages : en
Pages : 268

Book Description

Wartime Report

Wartime Report PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 834

Book Description
Reproductions of reports, some declassified, of research done at Langley Memorial Aeronautical Laboratory during World War II. The order of reports does not represent when they were chronologically issued. Reference to the original version of each report is included.

Wartime Report

Wartime Report PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 284

Book Description

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