Strut Support Interference On A Cylindrical Model With Boattail At Mach Numbers From 0 6 To 1 4

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Scientific And Technical Aerospace Reports

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Author :
language : en
Publisher:
Release Date : 1977

Scientific And Technical Aerospace Reports written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1977 with Aeronautics categories.

Sting Support Interference On Longitudinal Aerodynamic Characteristics Of Cargo Type Airplane Models At Mach 0 70 To 0 84

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Author : Donald L. Loving
language : en
Publisher:
Release Date : 1967

Sting Support Interference On Longitudinal Aerodynamic Characteristics Of Cargo Type Airplane Models At Mach 0 70 To 0 84 written by Donald L. Loving and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1967 with Airplanes categories.

Performance Of Convergent And Plug Nozzles At Mach Numbers From 0 To 1 97

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Author : Douglas E. Harrington
language : en
Publisher:
Release Date : 1970

Performance Of Convergent And Plug Nozzles At Mach Numbers From 0 To 1 97 written by Douglas E. Harrington and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1970 with categories.

Nasa Technical Note

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Author :
language : en
Publisher:
Release Date : 1967

Nasa Technical Note written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1967 with categories.

The Aeronautical Journal

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Author :
language : en
Publisher:
Release Date : 1990

The Aeronautical Journal written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1990 with Aeronautics categories.

Air Frame Propulsion Interference Papers And Discussion Of The Fluid Dynamics Panel Symposium Held At Rome 3 6 September 1974

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Author :
language : en
Publisher:
Release Date : 1975

Air Frame Propulsion Interference Papers And Discussion Of The Fluid Dynamics Panel Symposium Held At Rome 3 6 September 1974 written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1975 with Aerodynamics categories.

Drag Measurements From Different Wind Tunnels

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Author :
language : en
Publisher:
Release Date : 1966

Drag Measurements From Different Wind Tunnels written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1966 with categories.

Government Reports Annual Index

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Author :
language : en
Publisher:
Release Date : 199?

Government Reports Annual Index written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 199? with categories.

Critical Sting Length As Determined By The Measurement Of Pitch Damping Derivatives For Laminar Transitional And Turbulent Boundary Layers At Mach Number 3 For Reduced Frequencies Of 0 0033 And 0 0056

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Author : Bob L. Uselton
language : en
Publisher:
Release Date : 1977

Critical Sting Length As Determined By The Measurement Of Pitch Damping Derivatives For Laminar Transitional And Turbulent Boundary Layers At Mach Number 3 For Reduced Frequencies Of 0 0033 And 0 0056 written by Bob L. Uselton and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1977 with Pitching (Aerodynamics) categories.

A research program was initiated for the purpose of investigating some of the problem areas in regard to support interference in supersonic wind tunnels. The critical sting length at alpha = 0 was determined by the measurement of pitch-damping derivatives for laminar, transitional, and turbulent boundary layers at the model base. The effect of wedge splitter plates on sting interference was also investigated. By utilizing the small amplitude forced oscillation technique, data were obtained at Mach number 3 on a blunt 7-deg cone for reduced frequencies of 0.0033 and 0.0056. The results showed that the critical sting length with respect to sting interference on pitch-damping data was two model diameters for the two reduced frequencies investigated and was independent of the type of boundary layer at the model base. Decreasing the effective sting length from 3.3 to one model diameter increased the model base pressure substantially and the model surface pressure slightly. The critical sting length for minimal base pressure interference is 2.5 model diameters for this model and these test conditions.

Nasa Technical Paper

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Author :
language : en
Publisher:
Release Date : 1990

Nasa Technical Paper written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1990 with Astronautics categories.