Interference effects at transonic speeds of jets exhausting from the hull step of a model of a large, water-based airplane /

Wind-tunnel studies at subsonic and transonic speeds of a multiple-mission variable-wing- sweep airplane configuration /

Alford, William J.
Handerson, William P.
Luoma, Arvo A.
Langley Research Center.

January 1959

"November 1959."Cover title.Includes bibliographical references (p. 13).Mode of access: Internet

Interference between exhaust system and afterbody of twin-engine fuselage configurations /

Runckel, Jack F.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 16-17).Mode ...

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

Free-stream interference effects on effectiveness of control jets near the wing tip of a VTOL aircraft model /

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

January 1967

Cover title."August 1967."Includes bibliographical references (p. 8).Mode of access: Internet

Induced interference effects on a four-jet VTOL configuration with various wing planforms in the transition speed range /

Otis, James H.
United States. National Aeronautics and Space Administration.

Cover title."September 1962."Aerodynamics, aircraft; Aircraft; Stability and control.Includes biblio...

Interference effects of canard controls on the longitudinal aerodynamic characteristics of a winged body at Mach 10 /

Brooks, Cuyler W.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."April 1968."Includes bibliographical references (p. 11).Mode of access: Internet

Sting-support interference on longitudinal aerodynamic characteristics of cargo-type airplane models at Mach 0.70 to 0.84 /

Loving, Donald L.
Luoma, Arvo A.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."July 1967."Includes bibliographical references (p. 13).Mode of access: Internet

Transonic aerodynamic characteristics of a model of a proposed six-engine hull-type seaplane designed for supersonic flight /

Wornom, Dewey E.
United States. National Aeronautics and Space Administration.

"March 1960."Cover title.Includes bibliographical references (p. 9).Mode of access: Internet

Aerodynamic and hydrodynamic characteristics of a proposed supersonic multijet water-based hull-type airplane with a variable-incidence wing /

Petynia, William W.
Fournier, Roger H.
Pearson, Albin O.
United States. National Aeronautics and Space Administration.

"April 1960."Cover title.Includes bibliographical references (p. 10).Mode of access: Internet

The transonic aerodynamic characteristics of two variable-sweep airplane configurations capable of low-level supersonic attack /

Bielat, Ralph P.
Alford, William J.
Robins, A. Warner.
Langley Research Center.

January 1960

"August 1960."Cover title.Includes bibliographical references (p. 11-12).Mode of access: Internet

Transonic performance characteristics of several jet noise suppressors /

Schmeer, James W.
Cassetti, Marlowe D.
Salters, Leland B.
United States. National Aeronautics and Space Administration.

Cover title."July 1960."Aircraft; Aircraft safety and noise; Propulsion system elements.Includes bib...

Ground interference effects /

Schade, Robert O.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, aircraft; Stability and control.Includes bibliographical refe...

Hydrodynamic and aerodynamic characteristics of a model of a supersonic multijet water-based aircraft equipped with supercavitating hydrofoils /

McKann, Robert E.
Pearson, Albin O.
Blanchard, Ulysse J.
United States. National Aeronautics and Space Administration.

"February 1960."Cover title.Includes bibliographical references (p. 16).Mode of access: Internet

Effects of simulated rocket-jet exhaust on stability and control of a research-type airplane configuration at mach number of 6.86 /

Fetterman, David E.
United States. National Aeronautics and Space Administration.

"October 1959."Cover title.Includes bibliographical references (p. 15).Mode of access: Internet

Investigation of water-pond arresting of a dynamic model of a jet transport /

Thompson, William C.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Aircraft; Aircraft safety and noise; Piloting;Includes bibliographical refere...

Wind-tunnel studies at subsonic and transonic speeds of a multiple-mission variable-wing- sweep airplane configuration /

Alford, William J.
Handerson, William P.
Luoma, Arvo A.
Langley Research Center.

January 1959

"November 1959."Cover title.Includes bibliographical references (p. 13).Mode of access: Internet

Interference between exhaust system and afterbody of twin-engine fuselage configurations /

Runckel, Jack F.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 16-17).Mode ...

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

Free-stream interference effects on effectiveness of control jets near the wing tip of a VTOL aircraft model /

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

January 1967

Cover title."August 1967."Includes bibliographical references (p. 8).Mode of access: Internet

Induced interference effects on a four-jet VTOL configuration with various wing planforms in the transition speed range /

Otis, James H.
United States. National Aeronautics and Space Administration.

Cover title."September 1962."Aerodynamics, aircraft; Aircraft; Stability and control.Includes biblio...

Interference effects of canard controls on the longitudinal aerodynamic characteristics of a winged body at Mach 10 /

Brooks, Cuyler W.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."April 1968."Includes bibliographical references (p. 11).Mode of access: Internet

Sting-support interference on longitudinal aerodynamic characteristics of cargo-type airplane models at Mach 0.70 to 0.84 /

Loving, Donald L.
Luoma, Arvo A.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."July 1967."Includes bibliographical references (p. 13).Mode of access: Internet

Transonic aerodynamic characteristics of a model of a proposed six-engine hull-type seaplane designed for supersonic flight /

Wornom, Dewey E.
United States. National Aeronautics and Space Administration.

"March 1960."Cover title.Includes bibliographical references (p. 9).Mode of access: Internet

Aerodynamic and hydrodynamic characteristics of a proposed supersonic multijet water-based hull-type airplane with a variable-incidence wing /

Petynia, William W.
Fournier, Roger H.
Pearson, Albin O.
United States. National Aeronautics and Space Administration.

"April 1960."Cover title.Includes bibliographical references (p. 10).Mode of access: Internet

The transonic aerodynamic characteristics of two variable-sweep airplane configurations capable of low-level supersonic attack /

Bielat, Ralph P.
Alford, William J.
Robins, A. Warner.
Langley Research Center.

January 1960

"August 1960."Cover title.Includes bibliographical references (p. 11-12).Mode of access: Internet

Transonic performance characteristics of several jet noise suppressors /

Schmeer, James W.
Cassetti, Marlowe D.
Salters, Leland B.
United States. National Aeronautics and Space Administration.

Cover title."July 1960."Aircraft; Aircraft safety and noise; Propulsion system elements.Includes bib...

Ground interference effects /

Schade, Robert O.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, aircraft; Stability and control.Includes bibliographical refe...

Hydrodynamic and aerodynamic characteristics of a model of a supersonic multijet water-based aircraft equipped with supercavitating hydrofoils /

McKann, Robert E.
Pearson, Albin O.
Blanchard, Ulysse J.
United States. National Aeronautics and Space Administration.

"February 1960."Cover title.Includes bibliographical references (p. 16).Mode of access: Internet

Effects of simulated rocket-jet exhaust on stability and control of a research-type airplane configuration at mach number of 6.86 /

Fetterman, David E.
United States. National Aeronautics and Space Administration.

"October 1959."Cover title.Includes bibliographical references (p. 15).Mode of access: Internet

Investigation of water-pond arresting of a dynamic model of a jet transport /

Thompson, William C.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Aircraft; Aircraft safety and noise; Piloting;Includes bibliographical refere...

Wind-tunnel studies at subsonic and transonic speeds of a multiple-mission variable-wing- sweep airplane configuration /

Alford, William J.
Handerson, William P.
Luoma, Arvo A.
Langley Research Center.

January 1959

"November 1959."Cover title.Includes bibliographical references (p. 13).Mode of access: Internet

Interference between exhaust system and afterbody of twin-engine fuselage configurations /

Runckel, Jack F.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 16-17).Mode ...

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

Interference effects at transonic speeds of jets exhausting from the hull step of a model of a large, water-based airplane /

Abstract

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Interference effects at transonic speeds of jets exhausting from the hull step of a model of a large, water-based airplane /

Abstract

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