A transonic investigation of changing indentation design Mach number on the aerodynamic characteristics of a 45 degree sweptback-wing-body combination designed for high performance /

Investigation at transonic speeds of the loading over a 40 degree sweptback wing having an aspect ratio of 3, a taper ratio of 0.2 and NACA 65A004 airfoil sections /

Runckel, Jack F.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Aerodynamics, aircraft; Aircraft; Stresses and loads.Includes bibliographical...

An investigation of wing and aileron loads due to deflected inboard and outboard ailerons on a 4-percent-thick 30 degree swepptback wing at transonic speeds

Whitcomb, Charles F.
Critzos, Chris C.
Brown, Philippa F.
United States. National Aeronautics and Space Administration.

Cover title."January 1961."Aerodynamics, aircraft; Aircraft; Stability and control; Stresses and loa...

Investigation of low-subsonic flight characteristics of a model of a hypersonic boost-glide configuration having a 78 degree delta wing /by /

Paulson, John W.
Shanks, Robert E.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Stability ...

Effects at Mach numbers of 1.61 and 2.01 of camber and twist on the aerodynamic characteristics of three swept wings having the same planform /

Landrum, Emma Jean.
Czarnecki, K. R.
United States. National Aeronautics and Space Administration.

Cover title."August 1961."Major NASA subject terms: Aerodynamics, aircraft; Stability and control.In...

Aerodynamic characteristics at a mach number of 3.10 of several fourth-stage shapes of the scout research vehicle /

Jaquet, Byron M.
United States. National Aeronautics and Space Administration.

Cover title."June 1961."Major NASA subject terms: Aerodynamics, missiles and space vehicles; Missile...

Aerodynamic characteristics of low-aspect-ratio wings in close proximity to the ground/

Fink, Marvin P.
Lastinger, James L.
United States. National Aeronautics and Space Administration.

Cover title."July 1961."Major NASA subject terms:Aerodynamics, aircraft; Aircraft; Stability and con...

Investigation of interference of a deflected jet with free stream and ground on aerodynamic characteristics of a semispan Delta-wing VTOL model /

Spreemann, Kenneth P.
United States. National Aeronautics and Space Administration.

Cover title."August 1961."Major NASA subject terms: Aerodynamics, aircraft; Aircraft; Propulsion sys...

Investigation of the low-subsonic stability and control characteristics of a free-flying model of a thick 70 degree Delta reentrry configuration /

Paulson, John W.
Shanks, Robert E.
United States. National Aeronautics and Space Administration.

Cover title."October 1961."Major NASA subject terms: Aerodynamics, missiles and space vehicles; Stab...

Boundary-layer transition on a group of blunt nose shapes at a mach number of 2.20 /

Jackson, Mary W.
Czatnecki, K. R.
United States. National Aeronautics and Space Administration.

Cover title."July 1961."Major NASA subject terms: Aerodynamics, aircraft; Aerodynamics, missiles and...

Transonic investigation of aerodynamic characteristics of a swept-wing fighter-airplane model with leading-edge droop in combination with outboard chord-extensions and notches /

Whitcomb, Charles F.
Norton, Harry T.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliographi...

Effects of control-feel configuration on airplane longitudinal control response /

Crane, Harold L.
Sommers, Robert W.
United States. National Aeronautics and Space Administration.

Cover title."October 1961."Major NASA subject terms: Aerodynamics, aircraft; Stability and control; ...

Wind-tunnel investigation of a balloon as a towed deceleration at mach numbers from 1.47 to 2.50 /

McShera, John T.
Keyes, J. Wayne.
United States. National Aeronautics and Space Administration.

Cover title."August 1961."Major NASA subject terms: Aerodynamics, missiles and space vehicles; Aircr...

Stability and control characteristics of a small-scale model of an ariel vehicle supported by two ducted fans /

Parlett, Lysle P.
United States. National Aeronautics and Space Administration.

Cover title."July 1961."Major NASA subject terms: Aerodynamics, aircraft; Aircraft; Stability and co...

Aerodynamic characteristics over a mach number range of 1.40 to 2.78 of a rocket-propelled airplane configuration having a low 52.2⁰ delta wing and an unswept horizontal tail. /

Kehlet, Alan B.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliographi...

Investigation of an axisymmetric internal compression inlet at a mach number of about 3.8 /

Lundell, John H.
Anderson, Lewis A.
Scherrer, Richard.
United States. National Aeronautics and Space Administration.

Cover title."June 1961."Major NASA subject terms: Aircraft; Propulsion system elements; Propulsion s...

Investigation at transonic speeds of the loading over a 40 degree sweptback wing having an aspect ratio of 3, a taper ratio of 0.2 and NACA 65A004 airfoil sections /

Runckel, Jack F.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Aerodynamics, aircraft; Aircraft; Stresses and loads.Includes bibliographical...

An investigation of wing and aileron loads due to deflected inboard and outboard ailerons on a 4-percent-thick 30 degree swepptback wing at transonic speeds

Whitcomb, Charles F.
Critzos, Chris C.
Brown, Philippa F.
United States. National Aeronautics and Space Administration.

Cover title."January 1961."Aerodynamics, aircraft; Aircraft; Stability and control; Stresses and loa...

Investigation of low-subsonic flight characteristics of a model of a hypersonic boost-glide configuration having a 78 degree delta wing /by /

Paulson, John W.
Shanks, Robert E.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Stability ...

Effects at Mach numbers of 1.61 and 2.01 of camber and twist on the aerodynamic characteristics of three swept wings having the same planform /

Landrum, Emma Jean.
Czarnecki, K. R.
United States. National Aeronautics and Space Administration.

Cover title."August 1961."Major NASA subject terms: Aerodynamics, aircraft; Stability and control.In...

Aerodynamic characteristics at a mach number of 3.10 of several fourth-stage shapes of the scout research vehicle /

Jaquet, Byron M.
United States. National Aeronautics and Space Administration.

Cover title."June 1961."Major NASA subject terms: Aerodynamics, missiles and space vehicles; Missile...

Aerodynamic characteristics of low-aspect-ratio wings in close proximity to the ground/

Fink, Marvin P.
Lastinger, James L.
United States. National Aeronautics and Space Administration.

Cover title."July 1961."Major NASA subject terms:Aerodynamics, aircraft; Aircraft; Stability and con...

Investigation of interference of a deflected jet with free stream and ground on aerodynamic characteristics of a semispan Delta-wing VTOL model /

Spreemann, Kenneth P.
United States. National Aeronautics and Space Administration.

Cover title."August 1961."Major NASA subject terms: Aerodynamics, aircraft; Aircraft; Propulsion sys...

Investigation of the low-subsonic stability and control characteristics of a free-flying model of a thick 70 degree Delta reentrry configuration /

Paulson, John W.
Shanks, Robert E.
United States. National Aeronautics and Space Administration.

Cover title."October 1961."Major NASA subject terms: Aerodynamics, missiles and space vehicles; Stab...

Boundary-layer transition on a group of blunt nose shapes at a mach number of 2.20 /

Jackson, Mary W.
Czatnecki, K. R.
United States. National Aeronautics and Space Administration.

Cover title."July 1961."Major NASA subject terms: Aerodynamics, aircraft; Aerodynamics, missiles and...

Transonic investigation of aerodynamic characteristics of a swept-wing fighter-airplane model with leading-edge droop in combination with outboard chord-extensions and notches /

Whitcomb, Charles F.
Norton, Harry T.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliographi...

Effects of control-feel configuration on airplane longitudinal control response /

Crane, Harold L.
Sommers, Robert W.
United States. National Aeronautics and Space Administration.

Cover title."October 1961."Major NASA subject terms: Aerodynamics, aircraft; Stability and control; ...

Wind-tunnel investigation of a balloon as a towed deceleration at mach numbers from 1.47 to 2.50 /

McShera, John T.
Keyes, J. Wayne.
United States. National Aeronautics and Space Administration.

Cover title."August 1961."Major NASA subject terms: Aerodynamics, missiles and space vehicles; Aircr...

Stability and control characteristics of a small-scale model of an ariel vehicle supported by two ducted fans /

Parlett, Lysle P.
United States. National Aeronautics and Space Administration.

Cover title."July 1961."Major NASA subject terms: Aerodynamics, aircraft; Aircraft; Stability and co...

Aerodynamic characteristics over a mach number range of 1.40 to 2.78 of a rocket-propelled airplane configuration having a low 52.2⁰ delta wing and an unswept horizontal tail. /

Kehlet, Alan B.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliographi...

Investigation of an axisymmetric internal compression inlet at a mach number of about 3.8 /

Lundell, John H.
Anderson, Lewis A.
Scherrer, Richard.
United States. National Aeronautics and Space Administration.

Cover title."June 1961."Major NASA subject terms: Aircraft; Propulsion system elements; Propulsion s...

Investigation at transonic speeds of the loading over a 40 degree sweptback wing having an aspect ratio of 3, a taper ratio of 0.2 and NACA 65A004 airfoil sections /

Runckel, Jack F.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Aerodynamics, aircraft; Aircraft; Stresses and loads.Includes bibliographical...

An investigation of wing and aileron loads due to deflected inboard and outboard ailerons on a 4-percent-thick 30 degree swepptback wing at transonic speeds

Whitcomb, Charles F.
Critzos, Chris C.
Brown, Philippa F.
United States. National Aeronautics and Space Administration.

Cover title."January 1961."Aerodynamics, aircraft; Aircraft; Stability and control; Stresses and loa...

Investigation of low-subsonic flight characteristics of a model of a hypersonic boost-glide configuration having a 78 degree delta wing /by /

Paulson, John W.
Shanks, Robert E.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Stability ...

A transonic investigation of changing indentation design Mach number on the aerodynamic characteristics of a 45 degree sweptback-wing-body combination designed for high performance /

Abstract

Extracted data

A transonic investigation of changing indentation design Mach number on the aerodynamic characteristics of a 45 degree sweptback-wing-body combination designed for high performance /

Abstract

Extracted data

Related items

Related items