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An Analysis of the Stability and Control Characteristics of an Ejector Wing V/STOL During Transition

Title: An Analysis of the Stability and Control Characteristics of an Ejector Wing V/STOL During Transition
Date: 1973
Index Abstract: Coming Soon
Photo Quality: Complete
Report Number: AFFDL TR 72-37
Creator: Kurylowich, George; Martin, James M.
Corporate Author: Air Force Flight Dynamics Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Extent: 193
Identifier: AD0912045
Access Rights: Distribution Limited to U.S. Government Agencies
Distribution Classification: 1
Contract: Laboratory Research - No Contract
DoD Project: D095
DoD Task: None Given
DTIC Record Exists: No
Distribution Change Authority Correspondence: AFFDL LTR
Report Availability: Full text available
Date Issued: 1973-02
Abstract: The abstract for this report is either unavailable or has yet to be entered
Provenance: AFRL/VACA
Type: report
Format: 1 online resource