Effect of body-mounted lateral controls and speed brakes on the aerodynamic load distribution over a 45 degree swept wing at mach numbers from 0.80 to 0.98 /

Effects of deflected wing tips on the aerodynamic characteristics of a canard configuration at mach numbers from 0.7 to 3.5 /

Peterson, Victor L.
Bright, Loren G.
Ames Research Center.

January 1960

"September 1960."Cover title.Includes bibliographical references (p. 21).Mode of access: Internet

Flight investigation of the low-speed characteristics of a 45⁰ swept-wing fighter-type airplane with blowing boundary-layer control applied to the leading- and trailing-edge flaps

Quigley, Hervey C.
United States. National Aeronautics and Space Administration.

Cover title."September 1960."Aerodynamics, aircraft; Stability and control.Includes bibliographical ...

Normal-force and hinge-moment characteristics at transonic speeds of flap-type ailerons at three spanwise locations on a 4-percent-thick sweptback-wing-body model and pressure-distribution measurements on an inboard aileron. /

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

Cover title."May 1961."Aerodynamics, aircraft; Aircraft; Stability and control; Stresses and loads.I...

Spanwise loadings and aerodynamic characteristics for a series of trailing-edge controls on a 40° sweptback wing at Mach numbers of 1.61 and 2.01/

Landrum, Emma Jean.
Czarnecki, K. R.
Langley Research Center.

January 1962

"November 1962."Cover title.Includes bibliographical references (p. 9).Mode of access: Internet

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...

Effects of spoiler-slot-deflector control on the aerodynamic characteristics at a mach number of 2.01 of a variable-wing-sweep configuration with the outer wing panels swept back 75° /

Foster, Gerald V.
United States. National Aeronautics and Space Administration.

"April 1960."Cover title.Includes bibliographical references (p. 5).Mode of access: Internet

Effects of sweep angle on the boundary-layer stability characteristics of an untapered wing at low speeds /

Boltz, Frederick W.
Allen, Clyde Q.
Kenyon, George C.
United States. National Aeronautics and Space Administration.

Cover title."October 1960."Aerodynamics, aircraft; Fluid mechanics.Includes bibliographical referenc...

Span loadings and aerodynamic characteristics for a series of tip and trailing-edge controls on a 60° delta wing at Mach numbers of 1.61 and 2.01 /

Czarnecki, K. R.
Lord, Douglas R.
Langley Research Center.

January 1959

"September 1959."Cover title.Includes bibliographical references (p. 17-18).Mode of access: Internet

Static longitudinal and lateral aerodynamic characteristics at a Mach number of 2.20 of a variable-wing-sweep STOL configuration /

Foster, Gerald V.
Morris, Odell A.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1960

"October 1960."Cover title.Includes bibliographical references (p. 7-8).Mode of access: Internet

Flight investigation of some effects of a vane-controlled gust-alleviation system on the wing and tail loads fo a transport airplane /

Schott, Russell L.
United States. National Aeronautics and Space Administration.

Cover title."January 1961."Aerodynamics, aircraft; Aircraft; Aircraft safety and noise; Piloting; St...

The effects of thrust reversal at mach numbers up to 0.86 on the longitudinal and buffeting characteristics of a typical jet transport airplane configuration /

Sutton, Fred B.
Brownson, Jack J.
United States. National Aeronautics and Space Administration.

Cover title."March 1960."Mach number effects, complete wings;Wing, Nacelle combinations, airplanes; ...

The effects of an inverse-taper leading-edge flap on the aerodynamic loading characteristics of a 45° sweptback wing at Mach numbers to 0.90 /

Demele, Fred A.
Ames Research Center.

January 1959

"NASA TN D-138.""Ames Research Center, Moffett Field, Calif.""December 1959."Title from cover.Includ...

Effects of wing incidence on the longitudinal trim characteristics of a cambered 70° delta-wing configuration at mach numbers 3.0 to 5.0 /

Ahtye, Warren F.
Ames Research Center.

January 1960

"September 1960."Cover title.Includes bibliographical references (p. 23).Mode of access: Internet

Aerodynamic load measurements and opening characteristics of automatic leading-edge slats on a 45 degree sweptback wing at transonic speeds /

Arabian, Donald D.
Reid, Charles F.
Runckel, Jack F.
United States. National Aeronautics and Space Administration.

Cover title."September 1961."Aircraft; Stresses and loads.Includes bibliographical references.Mode o...

A note on the drag due to lift of delta wings at mach numbers up to 2.0 /

Osborne, Robert S.
Kelly, Thomas C.
United States. National Aeronautics and Space Administration.

Cover title."November 1960."Aerodynamics, aircraft; Aircraft.Includes bibliographical references.Mod...

Effects of deflected wing tips on the aerodynamic characteristics of a canard configuration at mach numbers from 0.7 to 3.5 /

Peterson, Victor L.
Bright, Loren G.
Ames Research Center.

January 1960

"September 1960."Cover title.Includes bibliographical references (p. 21).Mode of access: Internet

Flight investigation of the low-speed characteristics of a 45⁰ swept-wing fighter-type airplane with blowing boundary-layer control applied to the leading- and trailing-edge flaps

Quigley, Hervey C.
United States. National Aeronautics and Space Administration.

Cover title."September 1960."Aerodynamics, aircraft; Stability and control.Includes bibliographical ...

Normal-force and hinge-moment characteristics at transonic speeds of flap-type ailerons at three spanwise locations on a 4-percent-thick sweptback-wing-body model and pressure-distribution measurements on an inboard aileron. /

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

Cover title."May 1961."Aerodynamics, aircraft; Aircraft; Stability and control; Stresses and loads.I...

Spanwise loadings and aerodynamic characteristics for a series of trailing-edge controls on a 40° sweptback wing at Mach numbers of 1.61 and 2.01/

Landrum, Emma Jean.
Czarnecki, K. R.
Langley Research Center.

January 1962

"November 1962."Cover title.Includes bibliographical references (p. 9).Mode of access: Internet

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...

Effects of spoiler-slot-deflector control on the aerodynamic characteristics at a mach number of 2.01 of a variable-wing-sweep configuration with the outer wing panels swept back 75° /

Foster, Gerald V.
United States. National Aeronautics and Space Administration.

"April 1960."Cover title.Includes bibliographical references (p. 5).Mode of access: Internet

Effects of sweep angle on the boundary-layer stability characteristics of an untapered wing at low speeds /

Boltz, Frederick W.
Allen, Clyde Q.
Kenyon, George C.
United States. National Aeronautics and Space Administration.

Cover title."October 1960."Aerodynamics, aircraft; Fluid mechanics.Includes bibliographical referenc...

Span loadings and aerodynamic characteristics for a series of tip and trailing-edge controls on a 60° delta wing at Mach numbers of 1.61 and 2.01 /

Czarnecki, K. R.
Lord, Douglas R.
Langley Research Center.

January 1959

"September 1959."Cover title.Includes bibliographical references (p. 17-18).Mode of access: Internet

Static longitudinal and lateral aerodynamic characteristics at a Mach number of 2.20 of a variable-wing-sweep STOL configuration /

Foster, Gerald V.
Morris, Odell A.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1960

"October 1960."Cover title.Includes bibliographical references (p. 7-8).Mode of access: Internet

Flight investigation of some effects of a vane-controlled gust-alleviation system on the wing and tail loads fo a transport airplane /

Schott, Russell L.
United States. National Aeronautics and Space Administration.

Cover title."January 1961."Aerodynamics, aircraft; Aircraft; Aircraft safety and noise; Piloting; St...

The effects of thrust reversal at mach numbers up to 0.86 on the longitudinal and buffeting characteristics of a typical jet transport airplane configuration /

Sutton, Fred B.
Brownson, Jack J.
United States. National Aeronautics and Space Administration.

Cover title."March 1960."Mach number effects, complete wings;Wing, Nacelle combinations, airplanes; ...

The effects of an inverse-taper leading-edge flap on the aerodynamic loading characteristics of a 45° sweptback wing at Mach numbers to 0.90 /

Demele, Fred A.
Ames Research Center.

January 1959

"NASA TN D-138.""Ames Research Center, Moffett Field, Calif.""December 1959."Title from cover.Includ...

Effects of wing incidence on the longitudinal trim characteristics of a cambered 70° delta-wing configuration at mach numbers 3.0 to 5.0 /

Ahtye, Warren F.
Ames Research Center.

January 1960

"September 1960."Cover title.Includes bibliographical references (p. 23).Mode of access: Internet

Aerodynamic load measurements and opening characteristics of automatic leading-edge slats on a 45 degree sweptback wing at transonic speeds /

Arabian, Donald D.
Reid, Charles F.
Runckel, Jack F.
United States. National Aeronautics and Space Administration.

Cover title."September 1961."Aircraft; Stresses and loads.Includes bibliographical references.Mode o...

A note on the drag due to lift of delta wings at mach numbers up to 2.0 /

Osborne, Robert S.
Kelly, Thomas C.
United States. National Aeronautics and Space Administration.

Cover title."November 1960."Aerodynamics, aircraft; Aircraft.Includes bibliographical references.Mod...

Effects of deflected wing tips on the aerodynamic characteristics of a canard configuration at mach numbers from 0.7 to 3.5 /

Peterson, Victor L.
Bright, Loren G.
Ames Research Center.

January 1960

"September 1960."Cover title.Includes bibliographical references (p. 21).Mode of access: Internet

Flight investigation of the low-speed characteristics of a 45⁰ swept-wing fighter-type airplane with blowing boundary-layer control applied to the leading- and trailing-edge flaps

Quigley, Hervey C.
United States. National Aeronautics and Space Administration.

Cover title."September 1960."Aerodynamics, aircraft; Stability and control.Includes bibliographical ...

Normal-force and hinge-moment characteristics at transonic speeds of flap-type ailerons at three spanwise locations on a 4-percent-thick sweptback-wing-body model and pressure-distribution measurements on an inboard aileron. /

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

Cover title."May 1961."Aerodynamics, aircraft; Aircraft; Stability and control; Stresses and loads.I...

Effect of body-mounted lateral controls and speed brakes on the aerodynamic load distribution over a 45 degree swept wing at mach numbers from 0.80 to 0.98 /

Abstract

Extracted data

Effect of body-mounted lateral controls and speed brakes on the aerodynamic load distribution over a 45 degree swept wing at mach numbers from 0.80 to 0.98 /

Abstract

Extracted data

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