Author: Joseph W. Cleary
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 48
Book Description
Numerical solutions of the pressure distributions of blunt wedges for Mach numbers of 10 and ∞ are presented. The pressure distributions have been integrated to provide the inviscid lift, drag, and pitching-moment coefficients of any circularly blunt-wedge airfoil. The effects of varying surface angle, nose bluntness, and gas specific-heat ratio are discussed. A hypersonic wedge theory, derived from explicit oblique-shock equations, is introduced and is shown to predict accurately the loading and aerodynamic characteristics of surfaces with attached shocks. With appropriate account taken for nose bluntness, the theory is shown to be applicable to blunt airfoils.
Theoretical Aerodynamic Characteristics of Sharp and Circularly Blunt-wedge Airfoils
Author: Joseph W. Cleary
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 48
Book Description
Numerical solutions of the pressure distributions of blunt wedges for Mach numbers of 10 and ∞ are presented. The pressure distributions have been integrated to provide the inviscid lift, drag, and pitching-moment coefficients of any circularly blunt-wedge airfoil. The effects of varying surface angle, nose bluntness, and gas specific-heat ratio are discussed. A hypersonic wedge theory, derived from explicit oblique-shock equations, is introduced and is shown to predict accurately the loading and aerodynamic characteristics of surfaces with attached shocks. With appropriate account taken for nose bluntness, the theory is shown to be applicable to blunt airfoils.
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 48
Book Description
Numerical solutions of the pressure distributions of blunt wedges for Mach numbers of 10 and ∞ are presented. The pressure distributions have been integrated to provide the inviscid lift, drag, and pitching-moment coefficients of any circularly blunt-wedge airfoil. The effects of varying surface angle, nose bluntness, and gas specific-heat ratio are discussed. A hypersonic wedge theory, derived from explicit oblique-shock equations, is introduced and is shown to predict accurately the loading and aerodynamic characteristics of surfaces with attached shocks. With appropriate account taken for nose bluntness, the theory is shown to be applicable to blunt airfoils.
NASA Technical Report
An Experimental and Theoretical Investigation of the Pressure Distribution and Flow Fields of Blunted Cones at Hypersonic Mach Number
Author: Joseph W. Cleary
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 82
Book Description
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 82
Book Description
NASA Scientific and Technical Reports
Author: United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1152
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1152
Book Description
NASA Technical Note
Hypersonic Aerodynamic Characteristics of the Ames M-2 Lifting Entry Configuration
A Selected Listing of NASA Scientific and Technical Reports for ...
Scientific and Technical Aerospace Reports
Index Aeronauticus
Monthly Catalog of United States Government Publications
Author: United States. Superintendent of Documents
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1714
Book Description
February issue includes Appendix entitled Directory of United States Government periodicals and subscription publications; September issue includes List of depository libraries; June and December issues include semiannual index.
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1714
Book Description
February issue includes Appendix entitled Directory of United States Government periodicals and subscription publications; September issue includes List of depository libraries; June and December issues include semiannual index.