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Delta
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Gun Tunnel Force Measurements on Some Thin delta Wings Suitable for Hypersonic Cruising Flight
G T-2 Flight Test Data. Book XII - Timing, Pressure and Altitude Comparisons
Ground Effects Related to Landing of Airplanes with Low-Aspect-Ratio Wings
Geostationary Operational Environmental Satellite (GOES-F) Mission Operation Report
Geostationary Operational Environmental Satellite (GOES-C) Mission Operation Report
Free Flight Model Measurements of the Longitudinal Stability of a Transonic Swept-Winged Aircraft
Flutter Analysis and Testing of Pairs of Aerodynamically Interfering delta Wings
Flow Visualization and Detailed Load Measurements Over a Maneuvering UCAV 1303
Flight Test Results for the F-16XL With a Digital Flight Control System
Flight Performance of Fw-4D Solid-Propellant Rocket Motor on delta 50 (Aimp-E)
Flight Mechanics Analysis of Dynamic Derivatives of the Dornier Variable Wind Tunnel Model
Flight Mechanical Analysis of Dynamic Derivatives of the Dornier Variation Wind Tunnel Model
Flight Investigation of the Low-Speed Handling Qualities of a Tailless Delta-Wing Fighter Airplane
Flight Investigation of the Aerodynamic Properties of an Ogee Wing
Flight Evaluation of the Factors which Influence the Selection of Landing Approach Speeds
Flight Avionics Sequencing Telemetry (FAST) DIV Latching Display
Finite Element Modeling and Optimization of Aerospace Structures
Federal Motor Vehicle Safety Standard No. 109 (Tires). Uniroyal, Incorporated
Federal Motor Vehicle Safety Standard No. 109 (Tires). Uniroyal Incorporated
Federal Motor Vehicle Safety Standard No. 109 (Tires). Uniroyal, Inc
Exploratory Investigation of the Aerodynamic Characteristics of a Biwing Vehicle at Mach 20.3
Exploratory Flow Measurements in the Wing-Body Junction of a Possible Mach Four Vehicle
Experimental Transonic Flutter Characteristics of Two 72 Deg-Sweep delta-Wing Models
Experimental Investigation of Transverse Jet Effects Related to Hypersonic Space Vehicles
Experimental Investigation of Forces on Simple Lifting Bodies in Rarefied Hypersonic Flow
Experimental and Computational Sonic Boom Assessment of Lockheed-Martin N+2 Low Boom Models