NASA VG V/STOL Fighters Studies from the early 1960s

[flateric]

Static longitudinal and lateral aerodynamic characteristics at a Mach number of 2.20 of a V STOL airplane configuration with a variable-sweep wing and with a skewed wing design

https://ntrs.nasa.gov/citations/19660013086
TM-X-521
"STATIC LONGITUDINAL AND LATERAL AERODYNAMIC CHARACTERISTICS AT A MACH NUMBER OF 2.20 OF A V/STOL AIRPLANE CONFIGURATION WITH A VARIABLE-SWEEP WING AND WITH A SKEWED WING DESIGN"

 

[flateric]

Another swing-wing thing from 1960

TM-X-321
Performance, stability, and control characteristics at transonic speeds of three V STOL airplane configurations with wings of variable sweep
https://ntrs.nasa.gov/citations/19660020171

 

[flateric]

More pics of third configuration

 

[hesham]

Hi,

http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19660030316_1966030316.pdf
TM-X- 812
"STABILITY AND CONTROL CHARACTERISTICS AT MACH NUMBERS OF 1.41 AND 2.20 OF A MULTIMISSION STOL CONFIGURATION WITH A VARIABLE-SKEW WING"

 

[hesham]

Hi,

and from 1961,it look like the Republic/Fokker D-24.
http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19660020177_1966020177.pdf
TM-X-527
"LONGITUDINAL AERODYNAMIC CHARACTERISTICS AT TRANSONIC SPEEDS OF TWO V/STOL AIRPLANE CONFIGURATIONS WITH SKEWED AND V-SWEEP WINGS"

 

[overscan (PaulMM)]

Moved to own topic.

 

[overscan (PaulMM)]

Updated topic with fixed links and the names of reports in the posts.