Stephen W. D. Wolf

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Development of a quiet supersonic wind tunnel with a cryogenic adaptive nozzle

by Stephen W. D. Wolf First published in 1991 — 4 editions

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NASA Ames Laminar Flow Supersonic Wind Tunnel (LFSWT) tests of a 10 ̊cone at Mach 1.6

by Stephen W. D. Wolf First published in 1997 — 2 editions

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Adaptive wall technology for minimization of wall interferences in transonic wind tunnels

by Stephen W. D. Wolf First published in 1988 — 1 edition

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Highlights of experience with a flexible walled test section in the NASA Langley 0.3 meter transonic cryogenic tunnel

by Stephen W. D. Wolf First published in 1988 — 1 edition

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Predictive wall adjustment strategy for two-dimensional flexible walled adaptive wind tunnel: a detailed description of the first one-step method

by Stephen W. D. Wolf First published in 1988 — 1 edition

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Supersonic wind tunnel nozzles: a selected, annotated bibliography to aid in the development of quiet wind tunnel technology

by Stephen W. D. Wolf First published in 1990 — 1 edition

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Wall adjustment strategy software for use with the NASA Langley 0.3-meter transonic cryogenic tunnel adaptive wall test section

by Stephen W. D. Wolf First published in 1989 — 1 edition

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OLID: OL4661334A

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Created September 14, 2008
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September 14, 2008

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Stephen W. D. Wolf

7 works Add another?

Development of a quiet supersonic wind tunnel with a cryogenic adaptive nozzle

Create a new list

NASA Ames Laminar Flow Supersonic Wind Tunnel (LFSWT) tests of a 10 ̊cone at Mach 1.6

Adaptive wall technology for minimization of wall interferences in transonic wind tunnels

Highlights of experience with a flexible walled test section in the NASA Langley 0.3 meter transonic cryogenic tunnel

Predictive wall adjustment strategy for two-dimensional flexible walled adaptive wind tunnel: a detailed description of the first one-step method

Supersonic wind tunnel nozzles: a selected, annotated bibliography to aid in the development of quiet wind tunnel technology

Wall adjustment strategy software for use with the NASA Langley 0.3-meter transonic cryogenic tunnel adaptive wall test section

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