19th AIAA International Space Planes and Hypersonic Systems and Technologies Conference
Latest Publications

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Published By American Institute Of Aeronautics And Astronautics

9781624102844

Latest Documents Most Cited Documents Contributed Authors Related Sources Related Keywords

Startability analysis of Busemann intakes with overboard spillage

19th AIAA International Space Planes and Hypersonic Systems and Technologies Conference ◽

10.2514/6.2014-3227 ◽

2014 ◽

Author(s):

Niloofar Moradian ◽

Eugene Timofeev ◽

Rabi Tahir ◽

Sannu Molder

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Summary of Test Preparations for the Medium Scale Critical Components Test Program at the Aerodynamic and Propulsion Test Unit (Invited)

19th AIAA International Space Planes and Hypersonic Systems and Technologies Conference ◽

10.2514/6.2014-2482 ◽

2014 ◽

Cited By ~ 5

Author(s):

Sharon Rigney

Keyword(s):

Test Unit ◽

Test Program ◽

Medium Scale ◽

Critical Components

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Influence of Boundary Layer Transition on the Trajectory Optimisation of a Reusable Launch Vehicle

19th AIAA International Space Planes and Hypersonic Systems and Technologies Conference ◽

10.2514/6.2014-2362 ◽

2014 ◽

Cited By ~ 1

Author(s):

Romain Wuilbercq ◽

Fabrizio Pescetelli ◽

Edmondo Minisci ◽

Richard E. Brown

Keyword(s):

Boundary Layer ◽

Launch Vehicle ◽

Boundary Layer Transition ◽

Layer Transition ◽

Reusable Launch Vehicle ◽

Trajectory Optimisation

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Experimental research on thermal vibration characteristics of wing structure for high-speed flight vehicles in high-temperature environment

19th AIAA International Space Planes and Hypersonic Systems and Technologies Conference ◽

10.2514/6.2014-2511 ◽

2014 ◽

Author(s):

Dafang Wu ◽

Yuewu Wang ◽

Shougen Zhao ◽

Bing Pan ◽

Shuang Wu

Keyword(s):

High Temperature ◽

Experimental Research ◽

High Speed ◽

Vibration Characteristics ◽

Thermal Vibration ◽

Flight Vehicles ◽

Temperature Environment ◽

Wing Structure ◽

High Temperature Environment

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Characterization of a heterodyne LITA setup for simultaneous flow velocity and speed of sound measurements

19th AIAA International Space Planes and Hypersonic Systems and Technologies Conference ◽

10.2514/6.2014-2506 ◽

2014 ◽

Cited By ~ 2

Author(s):

Felix J. Förster ◽

Bernhard Weigand

Keyword(s):

Flow Velocity ◽

Speed Of Sound

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Design, Analyses, and Planned Calibration Tests for the Medium Scale Critical Components Direct Connect Facility Nozzles at the Aerodynamic and Propulsion Test Unit (Invited)

19th AIAA International Space Planes and Hypersonic Systems and Technologies Conference ◽

10.2514/6.2014-2485 ◽

2014 ◽

Cited By ~ 2

Author(s):

Kevin Holst

Keyword(s):

Test Unit ◽

Medium Scale ◽

Critical Components ◽

Design Analyses

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Multi-Phase Trajectory Optimisation for Access-to-Space with RBCC-Powered TSTO via Surrogated-Assisted Hybrid Evolutionary Algorithms Incorporating Pseudo-Spectral Methods

19th AIAA International Space Planes and Hypersonic Systems and Technologies Conference ◽

10.2514/6.2014-2360 ◽

2014 ◽

Cited By ~ 4

Author(s):

Hideaki Ogawa ◽

Masatoshi Kodera ◽

Sadatake Tomioka ◽

Shuichi Ueda

Keyword(s):

Evolutionary Algorithms ◽

Spectral Methods ◽

Phase Trajectory ◽

Hybrid Evolutionary Algorithms ◽

Multi Phase ◽

Pseudo Spectral ◽

Trajectory Optimisation

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Experimental Testing of an Airframe Integrated 3-D Scramjet at True Mach 10 Flight Conditions

19th AIAA International Space Planes and Hypersonic Systems and Technologies Conference ◽

10.2514/6.2014-2930 ◽

2014 ◽

Cited By ~ 1

Author(s):

Luke J. Doherty ◽

Michael Smart ◽

David Mee

Keyword(s):

Experimental Testing ◽

Mach 10

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Novel Hybrid Ablative/Ceramic Development for Re-Entry in Planetary Atmospheric Thermal Protection: Interfacial Adhesive Selection and Test Verification Plan

19th AIAA International Space Planes and Hypersonic Systems and Technologies Conference ◽

10.2514/6.2014-2373 ◽

2014 ◽

Cited By ~ 4

Author(s):

Jorge Barcena ◽

Sonia Florez ◽

Beatriz Perez ◽

Jean-Marc Bouilly ◽

Gregory Pinaud ◽

...

Keyword(s):

Thermal Protection ◽

Test Verification ◽

Verification Plan

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Effect of Initial Flight Path Angle Error and Control Constraint on the Optimized Ascent Trajectory of a Typical Launch Vehicle

19th AIAA International Space Planes and Hypersonic Systems and Technologies Conference ◽

10.2514/6.2014-2534 ◽

2014 ◽

Author(s):

Ashok Joshi ◽

B. Sudhir Kumar

Keyword(s):

Launch Vehicle ◽

Flight Path ◽

Control Constraint ◽

Angle Error ◽

Flight Path Angle ◽

And Control

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19th AIAA International Space Planes and Hypersonic Systems and Technologies ConferenceLatest Publications

TOTAL DOCUMENTS

H-INDEX

Published By American Institute Of Aeronautics And Astronautics

Startability analysis of Busemann intakes with overboard spillage

Summary of Test Preparations for the Medium Scale Critical Components Test Program at the Aerodynamic and Propulsion Test Unit (Invited)

Influence of Boundary Layer Transition on the Trajectory Optimisation of a Reusable Launch Vehicle

Experimental research on thermal vibration characteristics of wing structure for high-speed flight vehicles in high-temperature environment

Characterization of a heterodyne LITA setup for simultaneous flow velocity and speed of sound measurements

Design, Analyses, and Planned Calibration Tests for the Medium Scale Critical Components Direct Connect Facility Nozzles at the Aerodynamic and Propulsion Test Unit (Invited)

Multi-Phase Trajectory Optimisation for Access-to-Space with RBCC-Powered TSTO via Surrogated-Assisted Hybrid Evolutionary Algorithms Incorporating Pseudo-Spectral Methods

Experimental Testing of an Airframe Integrated 3-D Scramjet at True Mach 10 Flight Conditions

Novel Hybrid Ablative/Ceramic Development for Re-Entry in Planetary Atmospheric Thermal Protection: Interfacial Adhesive Selection and Test Verification Plan

Effect of Initial Flight Path Angle Error and Control Constraint on the Optimized Ascent Trajectory of a Typical Launch Vehicle

19th AIAA International Space Planes and Hypersonic Systems and Technologies Conference
Latest Publications