HYPERSONIC AND HIGH TEMPERATURE GAS DYNAMICS
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National Aeronautics and Space Administration An Overview of the Role of Systems Analysis in NASA's Hypersonics Project Jeffrey S. Robinson and John G. Martin NASA Langley Research Center, Hampton, VA Jeffrey V. Bowles and Unmeel B. Mehta NASA Ames -
NASA Aeronautics Directions URETI on Aeropropulsion and Power Technology Final Technical Forum Cleveland, OH October 16, 2007 Outline Program Overview Project Objectives / Goals and Technical Highlights The road ahead Outline Program Overview -
Two Separate Problems Design: to design the wing camber surface shape required to produce an optimum lifting-pressure distribution. Lift analysis: to define the lifting pressure distribution acting on a given wing camber-surface shape. Wings for S -
Space Access Vehicle Design - 2. HYPERSONIC MISSIONS IN THE LOWER ATMOSPHERE 2.1 The flight envelope The general aerodynamic and thermodynamic characteristics of the range of hypersonic missions carried out in the lower, sensible, atmosphere are sh -
Last Revised: February 12, 2009 Brief Summary of the Boeing/AFOSR Mach-6 Quiet Tunnel and Prof. Schneider's Research Professor Schneider's primary area of expertise is high-speed laminar-turbulent instability and transition. He focuses on hypersonic -
Propulsion Controls and Diagnostics Research at NASA GRC Status Report Dr. Sanjay Garg Branch Chief Ph: (216) 433-2685 FAX: (216) 433-8990 email: sanjay.garg@nasa.gov http:/www.lerc.nasa.gov/WWW/cdtb Presented at: Aerospace Guidance and Control Sys -
AA101 Study Guide (Sample Questions) History 1. What was the Montgolfier Brothers contribution to Aeronautics? Passenger carrying hot air balloon 2. Who is the father of Aerodynamics? Sir George Cayley 3. What German glider pilot proceeded the Wright -
Advanced propulsion systems (3 lectures) Hypersonic propulsion background (Lecture 1) Why hypersonic propulsion? Whats different at hypersonic conditions? What Real gas effects (non-constant CP, dissociation) Aircraft range How to compute t -
AME 436 Problem Set #7 Assigned: 4/30/08 "Due" 5/2/08 but no late penalty until 5/6/08, 12:00 noon; no assignments accepted after that date NO EXCEPTIONS! (Fax to me at 213-740-8071 if you're off campus.) NOTE: since your lowest homework grade wil -
AME 514 Applications of Combustion - Fall 2006 Final Exam 12/11/2006 Time allowed: 2 hours. Each problem is worth 25 points. Do any 4 of the 5 problems. You can try all of the problems, but turn in only 4 to be graded. The exam is open book and note -
Outline of Laminar-Turbulent Transition From A&AE 624/690T, Laminar-Turbulent Transition Prof. Steve Schneider, Purdue Univ. steves@ecn.purdue.edu, tel. 765-494-3343 last revised 19 August 2004 The following is an outline of the topics covered. While -
AA101: Air and Space Vehicles Final Review Final Exam 12/10/08 (Wed) 2:30 4:20 MEB 238 Closed Book/Note Course Outline 1/2 History of Aviation Airplane Design Aerodynamics Stability and Control Materials and Structures Airplane Propulsion 1 -
AME 514 Applications of Combustion - Fall 2004 Final Exam 12/9/2004 Time allowed: 2 hours. Each problem is worth 25 points. Do any 4 of the 6 problems. You can try all of the problems, but turn in only 4 to be graded. The exam is open book and notes -
Propulsion Challenges: Past, Present and Future Dr. Alan Garscadden Chief Scientist Propulsion Directorate Air Force Research Laboratory Propulsion Correlations Advances were made by prepared minds James Watt: latent heat concepts from Professo -
Major Hypersonic Ground Test Facilities The following brief summary is taken from "Advanced Hypersonic Test Facilities", edited by Frank Lu and Dan Marren, AIAA Progress in Astronautics and Aeronautics, v. 198, 2002. See also Kingsbury, "Aerospace