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Strake (aeronautics)
Vistara Soars Toward Expansion New Flight-Planning Technology Enhances Safety, Cuts Costs
United States Patent (19) 11) Patent Number: 4,691,879 Greene 45) Date of Patent: Sep
Water-Tunnel and Analytical Investigation of the Effect of Strake
4 INVENTOR 16%/6/S G
Aerodynamic Design of the Strake for the Rocket Plane in Tailless Configuration
Effect of Wing Planform and Canard Location and Geometry on the of a Close-Coupled Canard Wing
Aiaa-98-4448 Application of Forebody Strakes For
Technical Description
The Effect of Tailboom Strakes and Vertical Fin Modifications on the Performance and Handling Qualities of OH-58 Helicopters
The Discovery and Prediction of Vortex Flow Aerodynamics
Wing-Strake Juncture
Investigation of Empennage Buffeting
Computational Study of Flow Interactions Over a Close Coupled Canard-Wing on Fighter
Lateral-Directional Stability 6.7 Dynamic Lateral-Directional Stability 6.10 Stability and Control Analysis Example: F-16A and F-16C
'' Mr Cushion Landing Gear Applications Study "I
Effect of Actuated Forebody Strakes on the Forebody Aerodynamics of the NASA F-18 HARV
Dlr-Ib-As-Bs-2017-10
Master Thesis
Top View
Design and Integration of an Actuated Nose Strake Control System
United States Patent [19] [11] Patent Number: 4,739,957 Vess Et A1
Red Bull Air Racer
NASA-99-Isarvs-Bnp.Pdf
The Art of Soaring Flight
Helicopter Booster
Chapter 5 Wing Design
Fly Better Book 1 Aerodynamics
Configuration Heating for a Hypersonic Research Airplane Concept Having a 70" Swept Double-Delta Wing
Conceptual Design and Analysis of a High-Efficient Low-Emission Supersonic Aircraft HELESA
"'"L T I,...S~Go ~ 11
Design and Integration of an Actuated Nose Strake Control System
Bifurcation Flight Dynamic Analysis of a Strake-Wing Micro Aerial Vehicle
Modular Aeroplane System. a Concept and Initial Investigati On
PILOTS of CONTROL-IMPAIRED AIRCRAFT by ELAINE ANN
October Term, 1984
Aerodynamic of Forebody and Nose Strakes Based on F-16 Wind Tunnel Test Experience
Challenges & Needs for the Understanding of Combat Aircraft Aerodynamics
The Airframe Noise Reduction Challenge
Lockheed SR-71 Blackbird-EN
Aerodynamic Pitch-Up of Cranked Arrow Wings: Estimation, Trim, and Configuration Design
NI\SI\ National Aeronautics and Space Administration NASA Technical Memorandum 88354
Pre-Paint>Fuselage>Empennage>Fit Vertical Tail Fin Objectives of This Task
Flow Structure Past a Canonical Shape of Engine/Pylon/Wing Installation for Takeoff/Landing Conditions
Canard-Wing Interference Effects on the Flight Characteristics of a Transonic Passenger Aircraft
Chapter 6 Tail Design
NASA Facts National Aeronautics and Space Administration
Sb7man-SN5515-Onwards.Pdf
Aircraft Configuration Design Options
5M Configuration Evaluation and Testing
Annual Report 2014/15 | PDF 10.03 MB
National Oceanic and Atmospheric Administration (NOAA) Heritage Assets Database, 2019
In-Flight Lift-Drag Characteristics for a Forward-Swept-Wing Aircraft (And Comparisions with Contemporary Aircraft)
Preparations for Flight Research to Evaluate Actuated Forebody Strakes on the F-18 High-Alpha Research Vehicle
Effects of Nose Strakes on Transport Aircraft Student: Calvin T. Locklear
Vortex Dynamics Study and Flow Visualization on Aircraft Model with Different Canard Configurations
Better Performance Starts with Better Technology
High Angle of Attack Aerodynamics
Annex II: 3Rd Call for Proposals (CFP03): List and Full Description of Topics Call Text
Preparations for Flight Research to Evaluate Actuated Forebody Strakes on the F-18 High-Alpha Research Vehicle
UNSTEADY AERODYNAMIC ANALYSIS of SPACE SHUTTLE VEHICLES Part I: SUMMARY REPORT
ENGINEERING: a SPECIAL BIBLIOGRAPHY with INDEXES, SUPPLEMENT 48 (NASA) 92 P HC $.00 CSCL 01A Unclas 00/02 02213 AERONAUTICAL ENGINEERING