now it's clear that it's not AMSA-related
Title: Stability and control characteristics at Mach numbers of 1.41 and 2.20 of a multimission STOL airplane configuration with a variable-skew wing
Author(s): Foster, G. V.
Abstract: Stability and control characteristics at Mach numbers of 1.41 and 2.20 of multimission STOL AIRPLANE configuration with variable-skew wing
NASA Center: Langley Research Center
Publication Date: May 1, 1963
Document Source: CASI
Online Source: View PDF File
Document ID: 19660030316
Accession ID: 66N39606
Publication Information: Number of Pages = 69
Report Number: NASA-TM-X-812
Price Code: A04
Keywords: ANGLE OF ATTACK; BODY-WING CONFIGURATIONS; MACH NUMBER; SHORT TAKEOFF AIRCRAFT; STABILITY; SUPERSONIC SPEED; WINGS; BODY-WING COMBINATION; STABILITY AND CONTROL; STOL AIRCRAFT; SUPERSONIC SPEED;
Title: Aerodynamic characteristics at Mach numbers from 1.70 to 2.86 of a STOL model with a variable-skew wing
Author(s): Spearman, M. L.; Finch, V. M.
Abstract: No Abstract Available
NASA Center: Langley Research Center
Publication Date: Jan 1, 1964
Document Source: CASI
Online Source: View PDF File
Document ID: 19720065639
Accession ID: 72N73511
Publication Information: Number of Pages = 21
Report Number: L-3451; NASA-TM-X-903
Price Code: A03
Keywords: LATERAL STABILITY; LONGITUDINAL STABILITY; SHORT TAKEOFF AIRCRAFT; VARIABLE GEOMETRY STRUCTURES; SUPERSONIC FLOW;