Innovation in Flight: Research of the NASA Langley Research Center on Revolutionary Advanced Concepts for AeronauticsNational Aeronautics and Space Administration, 2005 - 389 pages |
Autres éditions - Tout afficher
Innovation in Flight: Research of the NASA Langley Research Center on ... Joseph R. Chambers Affichage du livre entier - 2005 |
Innovation in Flight: Research of the NASA Langley Research Center on ... Joseph R. Chambers Affichage du livre entier - 2005 |
Expressions et termes fréquents
active control aerodynamic aeroelastic Aeronautics AIAA Paper Air Force airplane airports angles of attack applications assessments aviation Blended Wing Body Boeing book contact capability challenges characteristics commercial concept conducted configuration control effectors control system cost Dryden dynamic effects efforts engine evaluations Flight Research flight tests flutter suppression fuel full-scale fuselage GPO Order Form GPO Stock Number high-speed HLFC industry joined-wing laminar flow Langley Research Center Langley's leading-edge lift loads low-speed Mach number Monograph in Aerospace nacelle NASA NASA's noise Online version available operations Order GPO Stock Personal Air Vehicle pilot potential powered-lift pressure propulsion reduced requirements runway incursion simulator sonic boom speed stability and control STOL structural studies subsonic suction supersonic cruise supersonic transport surface synthetic vision takeoff technical thrust vectoring trailing-edge Transonic Tunnel vehicle vortex flap wind-tunnel wind-tunnel tests wing
Fréquemment cités
Page 28 - It is my judgment that this Government should immediately commence a new program in partnership with private industry to develop at the earliest practical date the prototype of a commercially successful supersonic transport superior to that being built in any other country of the world .... Neither the economics nor the politics of international competition permits us to stand still in this area.
Page 344 - VOTEX-SYSTEM DETAILS OBTAINED ON F-106B AIRCRAFT USING A ROTATING VAPOR SCREEN AND SURFACE TECHNIQUES John E.
Page 337 - Flight Investigation of Boundary-Layer Control by Suction Slots on an NACA 35-215 Low-Drag Airfoil at High Reynolds Numbers.
Page 329 - USAF-NASAFAA Flight Program to Study Community Responses to Sonic Booms in the Greater St. Louis Area.
Page 329 - Wind-Tunnel/Flight Correlation Study of Aerodynamic Characteristics of a Large Flexible Supersonic Cruise Airplane (XB-70-1), Vol.
Page 69 - States of present and especially future foreign supersonic transport aircraft, and (3) to provide a sound technical basis for any future consideration that may be given by the United States to the development of an environmentally acceptable and economically viable commercial supersonic transport.
Page 330 - Runyan, LJ, Middleton, WD, and Paulson, JA, Wind Tunnel Test Results of a New Leading Edge Flap Design for Highly Swept Wings — A Vortex Flap, Supersonic Cruise Research 79, NASA CP-2108, Part 1, 1980, pp.
Page 62 - FY 2000 of $ 1 .0065 billion is focused on maximizing a return to our highest priority goals Aeronautics We are proud of our past accomplishments in two focused programs, High Speed Research (HSR) and Advanced Subsonic Technology (AST). Although dramatic advances were made against the original HSR program goals, our industry partners indicated that product development would be significantly delayed, which led to the decision to terminate this program in FY 1999.
Page 308 - These capabilities are: high-volume operations at airports without control towers or terminal radar facilities; lower adverse weather landing minimums at minimally equipped landing facilities; integration of SATS aircraft into a higher en route capacity air traffic control system with complex flows and slower aircraft; and improved...
Page 336 - NTIS 1979 Survey and Bibliography on Attainment of Laminar Flow Control in Air Using Pressure Gradient and .Suction...