17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference
Latest Publications

TOTAL DOCUMENTS

177

(FIVE YEARS 0)

H-INDEX

(FIVE YEARS 0)

Published By American Institute Of Aeronautics And Astronautics

9781600869426

Latest Documents Most Cited Documents Contributed Authors Related Sources Related Keywords

Orbiter Trajectory Analysis for a Two-Stage Reusable Launch Vehicle

17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference ◽

10.2514/6.2011-2370 ◽

2011 ◽

Author(s):

Adam Cowling

Keyword(s):

Trajectory Analysis ◽

Launch Vehicle ◽

Two Stage ◽

Reusable Launch Vehicle

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One-Dimensional Measurements of High Enthalpy Flow Temperature Using Spontaneous Raman Spectroscopy

17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference ◽

10.2514/6.2011-2212 ◽

2011 ◽

Cited By ~ 3

Author(s):

Stefan Hatzl ◽

Tobias Sander ◽

Christian Mundt

Keyword(s):

Raman Spectroscopy ◽

Flow Temperature ◽

One Dimensional ◽

High Enthalpy ◽

Dimensional Measurements

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Using the Vorticity Flux Equations to Model Hypersonic Transition

17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference ◽

10.2514/6.2011-2376 ◽

2011 ◽

Author(s):

David Nixon

Keyword(s):

Vorticity Flux

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Benchmark of Experimental Determination methods of Gas Permeabilities.

17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference ◽

10.2514/6.2011-2252 ◽

2011 ◽

Cited By ~ 1

Author(s):

Nicolas Gascoin ◽

Guillaume Fau ◽

Philippe Gillard ◽

Markus Kuhn ◽

Marc Bouchez ◽

...

Keyword(s):

Experimental Determination ◽

Determination Methods

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The SKYLON Project

17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference ◽

10.2514/6.2011-2244 ◽

2011 ◽

Cited By ~ 7

Author(s):

Roger Longstaff ◽

Alan Bond

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Numerical Investigation to Enhance the Thrust Vector of a Scramjet Nozzle

17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference ◽

10.2514/6.2011-2346 ◽

2011 ◽

Cited By ~ 2

Author(s):

Jan-Hendrik Meiss ◽

Wolfgang Schröder ◽

Matthias Meinke

Keyword(s):

Numerical Investigation ◽

Thrust Vector

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Preliminary Aerodynamic Shape Optimization of the SpaceLiner by Means of Engineering Methods

17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference ◽

10.2514/6.2011-2299 ◽

2011 ◽

Cited By ~ 7

Author(s):

Dominik Neeb ◽

Tobias Schwanekamp ◽

Ali Gülhan

Keyword(s):

Shape Optimization ◽

Aerodynamic Shape Optimization ◽

Aerodynamic Shape

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Experimental Investigation of the Material Response of Carbon Composite Ablators in the VKI Plasmatron Facility

17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference ◽

10.2514/6.2011-2302 ◽

2011 ◽

Cited By ~ 5

Author(s):

Bernd Helber ◽

Cem Asma ◽

Yacine Babou ◽

Thierry Magin ◽

O. Chazot

Keyword(s):

Experimental Investigation ◽

Carbon Composite ◽

Material Response

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Investigation of REST-class Hypersonic Inlet Designs

17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference ◽

10.2514/6.2011-2254 ◽

2011 ◽

Cited By ~ 15

Author(s):

Rowan Gollan ◽

Paul Ferlemann ◽

Paul Ferlemann

Keyword(s):

Hypersonic Inlet

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Design of Dual-Mode Engine Flowpaths for Hypersonic Vehicles Using Reduced-Order Models

17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference ◽

10.2514/6.2011-2380 ◽

2011 ◽

Cited By ~ 1

Author(s):

Sean Torrez ◽

Derek Dalle ◽

James Driscoll

Keyword(s):

Hypersonic Vehicles ◽

Reduced Order Models ◽

Dual Mode ◽

Reduced Order

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17th AIAA International Space Planes and Hypersonic Systems and Technologies ConferenceLatest Publications

TOTAL DOCUMENTS

H-INDEX

Published By American Institute Of Aeronautics And Astronautics

Orbiter Trajectory Analysis for a Two-Stage Reusable Launch Vehicle

One-Dimensional Measurements of High Enthalpy Flow Temperature Using Spontaneous Raman Spectroscopy

Using the Vorticity Flux Equations to Model Hypersonic Transition

Benchmark of Experimental Determination methods of Gas Permeabilities.

The SKYLON Project

Numerical Investigation to Enhance the Thrust Vector of a Scramjet Nozzle

Preliminary Aerodynamic Shape Optimization of the SpaceLiner by Means of Engineering Methods

Experimental Investigation of the Material Response of Carbon Composite Ablators in the VKI Plasmatron Facility

Investigation of REST-class Hypersonic Inlet Designs

Design of Dual-Mode Engine Flowpaths for Hypersonic Vehicles Using Reduced-Order Models

17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference
Latest Publications