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

flateric · 1 June 2007

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

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 - NASA Technical Reports Server (NTRS)

Static longitudinal and lateral aerodynamic characteristics of V/STOL aircraft with variable sweep wing

ntrs.nasa.gov

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 · 1 June 2007

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

Performance, stability, and control characteristics at transonic speeds of three V/STOL airplane configurations with wings of variable sweep - NASA Technical Reports Server (NTRS)

Performance, stability, and control of three V/STOL variable-wing-sweep aircraft configurations at transonic speeds

ntrs.nasa.gov

flateric · 1 June 2007

More pics of third configuration

hesham · 8 January 2009

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 · 16 February 2009

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) · 12 August 2010

Moved to own topic.

overscan (PaulMM) · 12 May 2022

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

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

flateric

ACCESS: USAP

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 - NASA Technical Reports Server (NTRS)

Attachments

flateric

ACCESS: USAP

Performance, stability, and control characteristics at transonic speeds of three V/STOL airplane configurations with wings of variable sweep - NASA Technical Reports Server (NTRS)

Attachments

flateric

ACCESS: USAP

Attachments

hesham

ACCESS: USAP

Attachments

hesham

ACCESS: USAP

Attachments

overscan (PaulMM)

Administrator

overscan (PaulMM)

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